
# decorator for wrapping every function
def client_wrap(func):
    def wrapper(*args, **kwargs):
        return _send_recieve(func.__name__, args, kwargs)
    return wrapper
# This file was automatically generated by SWIG (https://www.swig.org).
# Version 4.2.1
#
# Do not make changes to this file unless you know what you are doing - modify
# the SWIG interface file instead.

#
# This file has been modified by the OpenVSP automated facade script

from sys import version_info as _swig_python_version_info
# Import the low-level C/C++ module
if __package__ or "." in __name__:
    from . import _vsp
else:
    import _vsp

try:
    import builtins as __builtin__
except ImportError:
    import __builtin__

def _swig_repr(self):
    try:
        strthis = "proxy of " + self.this.__repr__()
    except __builtin__.Exception:
        strthis = ""
    return "<%s.%s; %s >" % (self.__class__.__module__, self.__class__.__name__, strthis,)


def _swig_setattr_nondynamic_instance_variable(set):
    def set_instance_attr(self, name, value):
        if name == "this":
            set(self, name, value)
        elif name == "thisown":
            self.this.own(value)
        elif hasattr(self, name) and isinstance(getattr(type(self), name), property):
            set(self, name, value)
        else:
            raise AttributeError("You cannot add instance attributes to %s" % self)
    return set_instance_attr


def _swig_setattr_nondynamic_class_variable(set):
    def set_class_attr(cls, name, value):
        if hasattr(cls, name) and not isinstance(getattr(cls, name), property):
            set(cls, name, value)
        else:
            raise AttributeError("You cannot add class attributes to %s" % cls)
    return set_class_attr


def _swig_add_metaclass(metaclass):
    """Class decorator for adding a metaclass to a SWIG wrapped class - a slimmed down version of six.add_metaclass"""
    def wrapper(cls):
        return metaclass(cls.__name__, cls.__bases__, cls.__dict__.copy())
    return wrapper


class _SwigNonDynamicMeta(type):
    """Meta class to enforce nondynamic attributes (no new attributes) for a class"""
    __setattr__ = _swig_setattr_nondynamic_class_variable(type.__setattr__)


class SwigPyIterator(object):
    thisown = property(lambda x: x.this.own(), lambda x, v: x.this.own(v), doc="The membership flag")

    def __init__(self, *args, **kwargs):
        raise AttributeError("No constructor defined - class is abstract")
    __repr__ = _swig_repr
    __swig_destroy__ = _vsp.delete_SwigPyIterator

    def value(self):
        return _vsp.SwigPyIterator_value(self)

    def incr(self, n=1):
        return _vsp.SwigPyIterator_incr(self, n)

    def decr(self, n=1):
        return _vsp.SwigPyIterator_decr(self, n)

    def distance(self, x):
        return _vsp.SwigPyIterator_distance(self, x)

    def equal(self, x):
        return _vsp.SwigPyIterator_equal(self, x)

    def copy(self):
        return _vsp.SwigPyIterator_copy(self)

    def next(self):
        return _vsp.SwigPyIterator_next(self)

    def __next__(self):
        return _vsp.SwigPyIterator___next__(self)

    def previous(self):
        return _vsp.SwigPyIterator_previous(self)

    def advance(self, n):
        return _vsp.SwigPyIterator_advance(self, n)

    def __eq__(self, x):
        return _vsp.SwigPyIterator___eq__(self, x)

    def __ne__(self, x):
        return _vsp.SwigPyIterator___ne__(self, x)

    def __iadd__(self, n):
        return _vsp.SwigPyIterator___iadd__(self, n)

    def __isub__(self, n):
        return _vsp.SwigPyIterator___isub__(self, n)

    def __add__(self, n):
        return _vsp.SwigPyIterator___add__(self, n)

    def __sub__(self, *args):
        return _vsp.SwigPyIterator___sub__(self, *args)
    def __iter__(self):
        return self

# Register SwigPyIterator in _vsp:
_vsp.SwigPyIterator_swigregister(SwigPyIterator)
class IntVector(object):
    thisown = property(lambda x: x.this.own(), lambda x, v: x.this.own(v), doc="The membership flag")
    __repr__ = _swig_repr

    def iterator(self):
        return _vsp.IntVector_iterator(self)
    def __iter__(self):
        return self.iterator()

    def __nonzero__(self):
        return _vsp.IntVector___nonzero__(self)

    def __bool__(self):
        return _vsp.IntVector___bool__(self)

    def __len__(self):
        return _vsp.IntVector___len__(self)

    def __getslice__(self, i, j):
        return _vsp.IntVector___getslice__(self, i, j)

    def __setslice__(self, *args):
        return _vsp.IntVector___setslice__(self, *args)

    def __delslice__(self, i, j):
        return _vsp.IntVector___delslice__(self, i, j)

    def __delitem__(self, *args):
        return _vsp.IntVector___delitem__(self, *args)

    def __getitem__(self, *args):
        return _vsp.IntVector___getitem__(self, *args)

    def __setitem__(self, *args):
        return _vsp.IntVector___setitem__(self, *args)

    def pop(self):
        return _vsp.IntVector_pop(self)

    def append(self, x):
        return _vsp.IntVector_append(self, x)

    def empty(self):
        return _vsp.IntVector_empty(self)

    def size(self):
        return _vsp.IntVector_size(self)

    def swap(self, v):
        return _vsp.IntVector_swap(self, v)

    def begin(self):
        return _vsp.IntVector_begin(self)

    def end(self):
        return _vsp.IntVector_end(self)

    def rbegin(self):
        return _vsp.IntVector_rbegin(self)

    def rend(self):
        return _vsp.IntVector_rend(self)

    def clear(self):
        return _vsp.IntVector_clear(self)

    def get_allocator(self):
        return _vsp.IntVector_get_allocator(self)

    def pop_back(self):
        return _vsp.IntVector_pop_back(self)

    def erase(self, *args):
        return _vsp.IntVector_erase(self, *args)

    def __init__(self, *args):
        _vsp.IntVector_swiginit(self, _vsp.new_IntVector(*args))

    def push_back(self, x):
        return _vsp.IntVector_push_back(self, x)

    def front(self):
        return _vsp.IntVector_front(self)

    def back(self):
        return _vsp.IntVector_back(self)

    def assign(self, n, x):
        return _vsp.IntVector_assign(self, n, x)

    def resize(self, *args):
        return _vsp.IntVector_resize(self, *args)

    def insert(self, *args):
        return _vsp.IntVector_insert(self, *args)

    def reserve(self, n):
        return _vsp.IntVector_reserve(self, n)

    def capacity(self):
        return _vsp.IntVector_capacity(self)
    __swig_destroy__ = _vsp.delete_IntVector

# Register IntVector in _vsp:
_vsp.IntVector_swigregister(IntVector)
class DoubleVector(object):
    thisown = property(lambda x: x.this.own(), lambda x, v: x.this.own(v), doc="The membership flag")
    __repr__ = _swig_repr

    def iterator(self):
        return _vsp.DoubleVector_iterator(self)
    def __iter__(self):
        return self.iterator()

    def __nonzero__(self):
        return _vsp.DoubleVector___nonzero__(self)

    def __bool__(self):
        return _vsp.DoubleVector___bool__(self)

    def __len__(self):
        return _vsp.DoubleVector___len__(self)

    def __getslice__(self, i, j):
        return _vsp.DoubleVector___getslice__(self, i, j)

    def __setslice__(self, *args):
        return _vsp.DoubleVector___setslice__(self, *args)

    def __delslice__(self, i, j):
        return _vsp.DoubleVector___delslice__(self, i, j)

    def __delitem__(self, *args):
        return _vsp.DoubleVector___delitem__(self, *args)

    def __getitem__(self, *args):
        return _vsp.DoubleVector___getitem__(self, *args)

    def __setitem__(self, *args):
        return _vsp.DoubleVector___setitem__(self, *args)

    def pop(self):
        return _vsp.DoubleVector_pop(self)

    def append(self, x):
        return _vsp.DoubleVector_append(self, x)

    def empty(self):
        return _vsp.DoubleVector_empty(self)

    def size(self):
        return _vsp.DoubleVector_size(self)

    def swap(self, v):
        return _vsp.DoubleVector_swap(self, v)

    def begin(self):
        return _vsp.DoubleVector_begin(self)

    def end(self):
        return _vsp.DoubleVector_end(self)

    def rbegin(self):
        return _vsp.DoubleVector_rbegin(self)

    def rend(self):
        return _vsp.DoubleVector_rend(self)

    def clear(self):
        return _vsp.DoubleVector_clear(self)

    def get_allocator(self):
        return _vsp.DoubleVector_get_allocator(self)

    def pop_back(self):
        return _vsp.DoubleVector_pop_back(self)

    def erase(self, *args):
        return _vsp.DoubleVector_erase(self, *args)

    def __init__(self, *args):
        _vsp.DoubleVector_swiginit(self, _vsp.new_DoubleVector(*args))

    def push_back(self, x):
        return _vsp.DoubleVector_push_back(self, x)

    def front(self):
        return _vsp.DoubleVector_front(self)

    def back(self):
        return _vsp.DoubleVector_back(self)

    def assign(self, n, x):
        return _vsp.DoubleVector_assign(self, n, x)

    def resize(self, *args):
        return _vsp.DoubleVector_resize(self, *args)

    def insert(self, *args):
        return _vsp.DoubleVector_insert(self, *args)

    def reserve(self, n):
        return _vsp.DoubleVector_reserve(self, n)

    def capacity(self):
        return _vsp.DoubleVector_capacity(self)
    __swig_destroy__ = _vsp.delete_DoubleVector

# Register DoubleVector in _vsp:
_vsp.DoubleVector_swigregister(DoubleVector)
class StringVector(object):
    thisown = property(lambda x: x.this.own(), lambda x, v: x.this.own(v), doc="The membership flag")
    __repr__ = _swig_repr

    def iterator(self):
        return _vsp.StringVector_iterator(self)
    def __iter__(self):
        return self.iterator()

    def __nonzero__(self):
        return _vsp.StringVector___nonzero__(self)

    def __bool__(self):
        return _vsp.StringVector___bool__(self)

    def __len__(self):
        return _vsp.StringVector___len__(self)

    def __getslice__(self, i, j):
        return _vsp.StringVector___getslice__(self, i, j)

    def __setslice__(self, *args):
        return _vsp.StringVector___setslice__(self, *args)

    def __delslice__(self, i, j):
        return _vsp.StringVector___delslice__(self, i, j)

    def __delitem__(self, *args):
        return _vsp.StringVector___delitem__(self, *args)

    def __getitem__(self, *args):
        return _vsp.StringVector___getitem__(self, *args)

    def __setitem__(self, *args):
        return _vsp.StringVector___setitem__(self, *args)

    def pop(self):
        return _vsp.StringVector_pop(self)

    def append(self, x):
        return _vsp.StringVector_append(self, x)

    def empty(self):
        return _vsp.StringVector_empty(self)

    def size(self):
        return _vsp.StringVector_size(self)

    def swap(self, v):
        return _vsp.StringVector_swap(self, v)

    def begin(self):
        return _vsp.StringVector_begin(self)

    def end(self):
        return _vsp.StringVector_end(self)

    def rbegin(self):
        return _vsp.StringVector_rbegin(self)

    def rend(self):
        return _vsp.StringVector_rend(self)

    def clear(self):
        return _vsp.StringVector_clear(self)

    def get_allocator(self):
        return _vsp.StringVector_get_allocator(self)

    def pop_back(self):
        return _vsp.StringVector_pop_back(self)

    def erase(self, *args):
        return _vsp.StringVector_erase(self, *args)

    def __init__(self, *args):
        _vsp.StringVector_swiginit(self, _vsp.new_StringVector(*args))

    def push_back(self, x):
        return _vsp.StringVector_push_back(self, x)

    def front(self):
        return _vsp.StringVector_front(self)

    def back(self):
        return _vsp.StringVector_back(self)

    def assign(self, n, x):
        return _vsp.StringVector_assign(self, n, x)

    def resize(self, *args):
        return _vsp.StringVector_resize(self, *args)

    def insert(self, *args):
        return _vsp.StringVector_insert(self, *args)

    def reserve(self, n):
        return _vsp.StringVector_reserve(self, n)

    def capacity(self):
        return _vsp.StringVector_capacity(self)
    __swig_destroy__ = _vsp.delete_StringVector

# Register StringVector in _vsp:
_vsp.StringVector_swigregister(StringVector)
class BoolVector(object):
    thisown = property(lambda x: x.this.own(), lambda x, v: x.this.own(v), doc="The membership flag")
    __repr__ = _swig_repr

    def iterator(self):
        return _vsp.BoolVector_iterator(self)
    def __iter__(self):
        return self.iterator()

    def __nonzero__(self):
        return _vsp.BoolVector___nonzero__(self)

    def __bool__(self):
        return _vsp.BoolVector___bool__(self)

    def __len__(self):
        return _vsp.BoolVector___len__(self)

    def __getslice__(self, i, j):
        return _vsp.BoolVector___getslice__(self, i, j)

    def __setslice__(self, *args):
        return _vsp.BoolVector___setslice__(self, *args)

    def __delslice__(self, i, j):
        return _vsp.BoolVector___delslice__(self, i, j)

    def __delitem__(self, *args):
        return _vsp.BoolVector___delitem__(self, *args)

    def __getitem__(self, *args):
        return _vsp.BoolVector___getitem__(self, *args)

    def __setitem__(self, *args):
        return _vsp.BoolVector___setitem__(self, *args)

    def pop(self):
        return _vsp.BoolVector_pop(self)

    def append(self, x):
        return _vsp.BoolVector_append(self, x)

    def empty(self):
        return _vsp.BoolVector_empty(self)

    def size(self):
        return _vsp.BoolVector_size(self)

    def swap(self, v):
        return _vsp.BoolVector_swap(self, v)

    def begin(self):
        return _vsp.BoolVector_begin(self)

    def end(self):
        return _vsp.BoolVector_end(self)

    def rbegin(self):
        return _vsp.BoolVector_rbegin(self)

    def rend(self):
        return _vsp.BoolVector_rend(self)

    def clear(self):
        return _vsp.BoolVector_clear(self)

    def get_allocator(self):
        return _vsp.BoolVector_get_allocator(self)

    def pop_back(self):
        return _vsp.BoolVector_pop_back(self)

    def erase(self, *args):
        return _vsp.BoolVector_erase(self, *args)

    def __init__(self, *args):
        _vsp.BoolVector_swiginit(self, _vsp.new_BoolVector(*args))

    def push_back(self, x):
        return _vsp.BoolVector_push_back(self, x)

    def front(self):
        return _vsp.BoolVector_front(self)

    def back(self):
        return _vsp.BoolVector_back(self)

    def assign(self, n, x):
        return _vsp.BoolVector_assign(self, n, x)

    def resize(self, *args):
        return _vsp.BoolVector_resize(self, *args)

    def insert(self, *args):
        return _vsp.BoolVector_insert(self, *args)

    def reserve(self, n):
        return _vsp.BoolVector_reserve(self, n)

    def capacity(self):
        return _vsp.BoolVector_capacity(self)
    __swig_destroy__ = _vsp.delete_BoolVector

# Register BoolVector in _vsp:
_vsp.BoolVector_swigregister(BoolVector)
class DoubleVecVec(object):
    thisown = property(lambda x: x.this.own(), lambda x, v: x.this.own(v), doc="The membership flag")
    __repr__ = _swig_repr

    def iterator(self):
        return _vsp.DoubleVecVec_iterator(self)
    def __iter__(self):
        return self.iterator()

    def __nonzero__(self):
        return _vsp.DoubleVecVec___nonzero__(self)

    def __bool__(self):
        return _vsp.DoubleVecVec___bool__(self)

    def __len__(self):
        return _vsp.DoubleVecVec___len__(self)

    def __getslice__(self, i, j):
        return _vsp.DoubleVecVec___getslice__(self, i, j)

    def __setslice__(self, *args):
        return _vsp.DoubleVecVec___setslice__(self, *args)

    def __delslice__(self, i, j):
        return _vsp.DoubleVecVec___delslice__(self, i, j)

    def __delitem__(self, *args):
        return _vsp.DoubleVecVec___delitem__(self, *args)

    def __getitem__(self, *args):
        return _vsp.DoubleVecVec___getitem__(self, *args)

    def __setitem__(self, *args):
        return _vsp.DoubleVecVec___setitem__(self, *args)

    def pop(self):
        return _vsp.DoubleVecVec_pop(self)

    def append(self, x):
        return _vsp.DoubleVecVec_append(self, x)

    def empty(self):
        return _vsp.DoubleVecVec_empty(self)

    def size(self):
        return _vsp.DoubleVecVec_size(self)

    def swap(self, v):
        return _vsp.DoubleVecVec_swap(self, v)

    def begin(self):
        return _vsp.DoubleVecVec_begin(self)

    def end(self):
        return _vsp.DoubleVecVec_end(self)

    def rbegin(self):
        return _vsp.DoubleVecVec_rbegin(self)

    def rend(self):
        return _vsp.DoubleVecVec_rend(self)

    def clear(self):
        return _vsp.DoubleVecVec_clear(self)

    def get_allocator(self):
        return _vsp.DoubleVecVec_get_allocator(self)

    def pop_back(self):
        return _vsp.DoubleVecVec_pop_back(self)

    def erase(self, *args):
        return _vsp.DoubleVecVec_erase(self, *args)

    def __init__(self, *args):
        _vsp.DoubleVecVec_swiginit(self, _vsp.new_DoubleVecVec(*args))

    def push_back(self, x):
        return _vsp.DoubleVecVec_push_back(self, x)

    def front(self):
        return _vsp.DoubleVecVec_front(self)

    def back(self):
        return _vsp.DoubleVecVec_back(self)

    def assign(self, n, x):
        return _vsp.DoubleVecVec_assign(self, n, x)

    def resize(self, *args):
        return _vsp.DoubleVecVec_resize(self, *args)

    def insert(self, *args):
        return _vsp.DoubleVecVec_insert(self, *args)

    def reserve(self, n):
        return _vsp.DoubleVecVec_reserve(self, n)

    def capacity(self):
        return _vsp.DoubleVecVec_capacity(self)
    __swig_destroy__ = _vsp.delete_DoubleVecVec

# Register DoubleVecVec in _vsp:
_vsp.DoubleVecVec_swigregister(DoubleVecVec)
class Vec3dVec(object):
    thisown = property(lambda x: x.this.own(), lambda x, v: x.this.own(v), doc="The membership flag")
    __repr__ = _swig_repr

    def iterator(self):
        return _vsp.Vec3dVec_iterator(self)
    def __iter__(self):
        return self.iterator()

    def __nonzero__(self):
        return _vsp.Vec3dVec___nonzero__(self)

    def __bool__(self):
        return _vsp.Vec3dVec___bool__(self)

    def __len__(self):
        return _vsp.Vec3dVec___len__(self)

    def __getslice__(self, i, j):
        return _vsp.Vec3dVec___getslice__(self, i, j)

    def __setslice__(self, *args):
        return _vsp.Vec3dVec___setslice__(self, *args)

    def __delslice__(self, i, j):
        return _vsp.Vec3dVec___delslice__(self, i, j)

    def __delitem__(self, *args):
        return _vsp.Vec3dVec___delitem__(self, *args)

    def __getitem__(self, *args):
        return _vsp.Vec3dVec___getitem__(self, *args)

    def __setitem__(self, *args):
        return _vsp.Vec3dVec___setitem__(self, *args)

    def pop(self):
        return _vsp.Vec3dVec_pop(self)

    def append(self, x):
        return _vsp.Vec3dVec_append(self, x)

    def empty(self):
        return _vsp.Vec3dVec_empty(self)

    def size(self):
        return _vsp.Vec3dVec_size(self)

    def swap(self, v):
        return _vsp.Vec3dVec_swap(self, v)

    def begin(self):
        return _vsp.Vec3dVec_begin(self)

    def end(self):
        return _vsp.Vec3dVec_end(self)

    def rbegin(self):
        return _vsp.Vec3dVec_rbegin(self)

    def rend(self):
        return _vsp.Vec3dVec_rend(self)

    def clear(self):
        return _vsp.Vec3dVec_clear(self)

    def get_allocator(self):
        return _vsp.Vec3dVec_get_allocator(self)

    def pop_back(self):
        return _vsp.Vec3dVec_pop_back(self)

    def erase(self, *args):
        return _vsp.Vec3dVec_erase(self, *args)

    def __init__(self, *args):
        _vsp.Vec3dVec_swiginit(self, _vsp.new_Vec3dVec(*args))

    def push_back(self, x):
        return _vsp.Vec3dVec_push_back(self, x)

    def front(self):
        return _vsp.Vec3dVec_front(self)

    def back(self):
        return _vsp.Vec3dVec_back(self)

    def assign(self, n, x):
        return _vsp.Vec3dVec_assign(self, n, x)

    def resize(self, *args):
        return _vsp.Vec3dVec_resize(self, *args)

    def insert(self, *args):
        return _vsp.Vec3dVec_insert(self, *args)

    def reserve(self, n):
        return _vsp.Vec3dVec_reserve(self, n)

    def capacity(self):
        return _vsp.Vec3dVec_capacity(self)
    __swig_destroy__ = _vsp.delete_Vec3dVec

# Register Vec3dVec in _vsp:
_vsp.Vec3dVec_swigregister(Vec3dVec)
class Matrix4dVec(object):
    thisown = property(lambda x: x.this.own(), lambda x, v: x.this.own(v), doc="The membership flag")
    __repr__ = _swig_repr

    def iterator(self):
        return _vsp.Matrix4dVec_iterator(self)
    def __iter__(self):
        return self.iterator()

    def __nonzero__(self):
        return _vsp.Matrix4dVec___nonzero__(self)

    def __bool__(self):
        return _vsp.Matrix4dVec___bool__(self)

    def __len__(self):
        return _vsp.Matrix4dVec___len__(self)

    def __getslice__(self, i, j):
        return _vsp.Matrix4dVec___getslice__(self, i, j)

    def __setslice__(self, *args):
        return _vsp.Matrix4dVec___setslice__(self, *args)

    def __delslice__(self, i, j):
        return _vsp.Matrix4dVec___delslice__(self, i, j)

    def __delitem__(self, *args):
        return _vsp.Matrix4dVec___delitem__(self, *args)

    def __getitem__(self, *args):
        return _vsp.Matrix4dVec___getitem__(self, *args)

    def __setitem__(self, *args):
        return _vsp.Matrix4dVec___setitem__(self, *args)

    def pop(self):
        return _vsp.Matrix4dVec_pop(self)

    def append(self, x):
        return _vsp.Matrix4dVec_append(self, x)

    def empty(self):
        return _vsp.Matrix4dVec_empty(self)

    def size(self):
        return _vsp.Matrix4dVec_size(self)

    def swap(self, v):
        return _vsp.Matrix4dVec_swap(self, v)

    def begin(self):
        return _vsp.Matrix4dVec_begin(self)

    def end(self):
        return _vsp.Matrix4dVec_end(self)

    def rbegin(self):
        return _vsp.Matrix4dVec_rbegin(self)

    def rend(self):
        return _vsp.Matrix4dVec_rend(self)

    def clear(self):
        return _vsp.Matrix4dVec_clear(self)

    def get_allocator(self):
        return _vsp.Matrix4dVec_get_allocator(self)

    def pop_back(self):
        return _vsp.Matrix4dVec_pop_back(self)

    def erase(self, *args):
        return _vsp.Matrix4dVec_erase(self, *args)

    def __init__(self, *args):
        _vsp.Matrix4dVec_swiginit(self, _vsp.new_Matrix4dVec(*args))

    def push_back(self, x):
        return _vsp.Matrix4dVec_push_back(self, x)

    def front(self):
        return _vsp.Matrix4dVec_front(self)

    def back(self):
        return _vsp.Matrix4dVec_back(self)

    def assign(self, n, x):
        return _vsp.Matrix4dVec_assign(self, n, x)

    def resize(self, *args):
        return _vsp.Matrix4dVec_resize(self, *args)

    def insert(self, *args):
        return _vsp.Matrix4dVec_insert(self, *args)

    def reserve(self, n):
        return _vsp.Matrix4dVec_reserve(self, n)

    def capacity(self):
        return _vsp.Matrix4dVec_capacity(self)
    __swig_destroy__ = _vsp.delete_Matrix4dVec

# Register Matrix4dVec in _vsp:
_vsp.Matrix4dVec_swigregister(Matrix4dVec)
ABS = _vsp.ABS
r""" Absolute position"""
REL = _vsp.REL
r""" Relative position"""
SELIG_AF_EXPORT = _vsp.SELIG_AF_EXPORT
r""" Selig airfoil file format"""
BEZIER_AF_EXPORT = _vsp.BEZIER_AF_EXPORT
r""" Bezier airfoil file format"""
ALIGN_LEFT = _vsp.ALIGN_LEFT
r""" Align to left"""
ALIGN_CENTER = _vsp.ALIGN_CENTER
r""" Align to center"""
ALIGN_RIGHT = _vsp.ALIGN_RIGHT
r""" Align to right"""
ALIGN_PIXEL = _vsp.ALIGN_PIXEL
r""" Align to specified pixel"""
ALIGN_TOP = _vsp.ALIGN_TOP
r""" Align to top"""
ALIGN_MIDDLE = _vsp.ALIGN_MIDDLE
r""" Align to middle"""
ALIGN_BOTTOM = _vsp.ALIGN_BOTTOM
r""" Align to bottom"""
NUM_ALIGN_TYPE = _vsp.NUM_ALIGN_TYPE
r""" Number of alignment types"""
ANG_RAD = _vsp.ANG_RAD
r""" Radians"""
ANG_DEG = _vsp.ANG_DEG
r""" Degrees"""
ANG_0 = _vsp.ANG_0
r""" Zero deg"""
ANG_90 = _vsp.ANG_90
r""" 90 deg"""
ANG_180 = _vsp.ANG_180
r""" 180 deg"""
ANG_270 = _vsp.ANG_270
r""" 270 deg"""
NUM_ANG = _vsp.NUM_ANG
r""" Number of angle choices"""
ATMOS_TYPE_US_STANDARD_1976 = _vsp.ATMOS_TYPE_US_STANDARD_1976
r""" US Standard Atmosphere 1976 (default)"""
ATMOS_TYPE_HERRINGTON_1966 = _vsp.ATMOS_TYPE_HERRINGTON_1966
r""" USAF 1966"""
ATMOS_TYPE_MANUAL_P_R = _vsp.ATMOS_TYPE_MANUAL_P_R
r""" Manual: pressure and density control"""
ATMOS_TYPE_MANUAL_P_T = _vsp.ATMOS_TYPE_MANUAL_P_T
r""" Manual: pressure and temperature control"""
ATMOS_TYPE_MANUAL_R_T = _vsp.ATMOS_TYPE_MANUAL_R_T
r""" Manual: density and temperature control"""
ATMOS_TYPE_MANUAL_RE_L = _vsp.ATMOS_TYPE_MANUAL_RE_L
r""" Manual: Reynolds number and length control"""
ATTACH_TRANS_NONE = _vsp.ATTACH_TRANS_NONE
r""" No parent attachment for translations"""
ATTACH_TRANS_COMP = _vsp.ATTACH_TRANS_COMP
r""" Translation relative to parent body axes"""
ATTACH_TRANS_UV = _vsp.ATTACH_TRANS_UV
r""" Translation relative to parent surface coordinate frame"""
ATTACH_TRANS_RST = _vsp.ATTACH_TRANS_RST
r""" Translation relative to parent per-section volume coordinate frame"""
ATTACH_TRANS_LMN = _vsp.ATTACH_TRANS_LMN
r""" Translation relative to parent uniform volume coordinate frame"""
ATTACH_TRANS_EtaMN = _vsp.ATTACH_TRANS_EtaMN
r""" Translation relative to wing parent uniform eta volume coordinate frame"""
ATTACH_TRANS_NUM_TYPES = _vsp.ATTACH_TRANS_NUM_TYPES
r""" Number of translation attachment types"""
ATTACH_ROT_NONE = _vsp.ATTACH_ROT_NONE
r""" No parent attachment for rotations"""
ATTACH_ROT_COMP = _vsp.ATTACH_ROT_COMP
r""" Rotation relative to parent body axes"""
ATTACH_ROT_UV = _vsp.ATTACH_ROT_UV
r""" Rotation relative to parent surface coordinate frame"""
ATTACH_ROT_RST = _vsp.ATTACH_ROT_RST
r""" Rotation relative to parent per-section volume coordinate frame"""
ATTACH_ROT_LMN = _vsp.ATTACH_ROT_LMN
r""" Rotation relative to parent uniform volume coordinate frame"""
ATTACH_ROT_EtaMN = _vsp.ATTACH_ROT_EtaMN
r""" Rotation relative to wing parent eta volume coordinate frame"""
ATTACH_ROT_NUM_TYPES = _vsp.ATTACH_ROT_NUM_TYPES
r""" Number of rotation attachment types"""
BOR_FLOWTHROUGH = _vsp.BOR_FLOWTHROUGH
r""" Flowthrough mode (default)"""
BOR_UPPER = _vsp.BOR_UPPER
r""" Upper surface mode"""
BOR_LOWER = _vsp.BOR_LOWER
r""" Lower surface mode"""
BOR_NUM_MODES = _vsp.BOR_NUM_MODES
r""" Number of Body of Revolution modes"""
MAX_CAMB = _vsp.MAX_CAMB
r""" Input maximum camber, calculate ideal lift coefficient"""
DESIGN_CL = _vsp.DESIGN_CL
r""" Input ideal lift coefficient, calculate maximum camber"""
NO_END_CAP = _vsp.NO_END_CAP
r""" No end cap"""
FLAT_END_CAP = _vsp.FLAT_END_CAP
r""" Flat end cap"""
ROUND_END_CAP = _vsp.ROUND_END_CAP
r""" Round end cap"""
EDGE_END_CAP = _vsp.EDGE_END_CAP
r""" Edge end cap"""
SHARP_END_CAP = _vsp.SHARP_END_CAP
r""" Sharp end cap"""
POINT_END_CAP = _vsp.POINT_END_CAP
ROUND_EXT_END_CAP_NONE = _vsp.ROUND_EXT_END_CAP_NONE
r""" Extended round end cap, but not extended"""
ROUND_EXT_END_CAP_LE = _vsp.ROUND_EXT_END_CAP_LE
r""" Extended round end cap, extend LE"""
ROUND_EXT_END_CAP_TE = _vsp.ROUND_EXT_END_CAP_TE
r""" Extended round end cap, extend TE"""
ROUND_EXT_END_CAP_BOTH = _vsp.ROUND_EXT_END_CAP_BOTH
r""" Extended round end cap, extend both"""
NUM_END_CAP_OPTIONS = _vsp.NUM_END_CAP_OPTIONS
r""" Number of end cap options"""
CFD_MIN_EDGE_LEN = _vsp.CFD_MIN_EDGE_LEN
r""" Minimum mesh edge length"""
CFD_MAX_EDGE_LEN = _vsp.CFD_MAX_EDGE_LEN
r""" Maximum mesh edge length"""
CFD_MAX_GAP = _vsp.CFD_MAX_GAP
r""" Maximum mesh edge gap"""
CFD_NUM_CIRCLE_SEGS = _vsp.CFD_NUM_CIRCLE_SEGS
r""" Number of edge segments to resolve circle"""
CFD_GROWTH_RATIO = _vsp.CFD_GROWTH_RATIO
r""" Maximum allowed edge growth ratio"""
CFD_LIMIT_GROWTH_FLAG = _vsp.CFD_LIMIT_GROWTH_FLAG
r""" Rigorous 3D growth limiting flag"""
CFD_INTERSECT_SUBSURFACE_FLAG = _vsp.CFD_INTERSECT_SUBSURFACE_FLAG
r""" Flag to intersect sub-surfaces"""
CFD_HALF_MESH_FLAG = _vsp.CFD_HALF_MESH_FLAG
r""" Flag to generate a half mesh"""
CFD_FAR_FIELD_FLAG = _vsp.CFD_FAR_FIELD_FLAG
r""" Flag to generate a far field mesh"""
CFD_FAR_MAX_EDGE_LEN = _vsp.CFD_FAR_MAX_EDGE_LEN
r""" Maximum far field mesh edge length"""
CFD_FAR_MAX_GAP = _vsp.CFD_FAR_MAX_GAP
r""" Maximum far field mesh edge gap"""
CFD_FAR_NUM_CIRCLE_SEGS = _vsp.CFD_FAR_NUM_CIRCLE_SEGS
r""" Number of far field edge segments to resolve circle"""
CFD_FAR_SIZE_ABS_FLAG = _vsp.CFD_FAR_SIZE_ABS_FLAG
r""" Relative or absolute size flag"""
CFD_FAR_LENGTH = _vsp.CFD_FAR_LENGTH
r""" Far field length"""
CFD_FAR_WIDTH = _vsp.CFD_FAR_WIDTH
r""" Far field width"""
CFD_FAR_HEIGHT = _vsp.CFD_FAR_HEIGHT
r""" Far field height"""
CFD_FAR_X_SCALE = _vsp.CFD_FAR_X_SCALE
r"""  Far field X scale"""
CFD_FAR_Y_SCALE = _vsp.CFD_FAR_Y_SCALE
r"""  Far field Y scale"""
CFD_FAR_Z_SCALE = _vsp.CFD_FAR_Z_SCALE
r"""  Far field Z scale"""
CFD_FAR_LOC_MAN_FLAG = _vsp.CFD_FAR_LOC_MAN_FLAG
r""" Far field location flag: centered or manual"""
CFD_FAR_LOC_X = _vsp.CFD_FAR_LOC_X
r""" Far field X location"""
CFD_FAR_LOC_Y = _vsp.CFD_FAR_LOC_Y
r""" Far field Y location"""
CFD_FAR_LOC_Z = _vsp.CFD_FAR_LOC_Z
r""" Far field Z location"""
CFD_SRF_XYZ_FLAG = _vsp.CFD_SRF_XYZ_FLAG
r""" Flag to include X,Y,Z intersection curves in export files"""
CFD_STL_FILE_NAME = _vsp.CFD_STL_FILE_NAME
r""" STL export type"""
CFD_POLY_FILE_NAME = _vsp.CFD_POLY_FILE_NAME
r""" POLY export type"""
CFD_TRI_FILE_NAME = _vsp.CFD_TRI_FILE_NAME
r""" TRI export type"""
CFD_OBJ_FILE_NAME = _vsp.CFD_OBJ_FILE_NAME
r""" OBJ export type"""
CFD_DAT_FILE_NAME = _vsp.CFD_DAT_FILE_NAME
r""" DAT export type"""
CFD_KEY_FILE_NAME = _vsp.CFD_KEY_FILE_NAME
r""" KEY export type"""
CFD_GMSH_FILE_NAME = _vsp.CFD_GMSH_FILE_NAME
r""" GMSH export type"""
CFD_TKEY_FILE_NAME = _vsp.CFD_TKEY_FILE_NAME
r""" TKEY export type"""
CFD_FACET_FILE_NAME = _vsp.CFD_FACET_FILE_NAME
r""" FACET export type"""
CFD_VSPGEOM_FILE_NAME = _vsp.CFD_VSPGEOM_FILE_NAME
r""" VSPGEOM export type"""
CFD_NUM_FILE_NAMES = _vsp.CFD_NUM_FILE_NAMES
r""" Number of CFD Mesh export file types"""
POINT_SOURCE = _vsp.POINT_SOURCE
r""" Point source"""
LINE_SOURCE = _vsp.LINE_SOURCE
r""" Line source"""
BOX_SOURCE = _vsp.BOX_SOURCE
r""" Box source"""
ULINE_SOURCE = _vsp.ULINE_SOURCE
r""" Constant U Line source"""
WLINE_SOURCE = _vsp.WLINE_SOURCE
r""" Constant W Line source"""
NUM_SOURCE_TYPES = _vsp.NUM_SOURCE_TYPES
r""" Number of CFD Mesh source types"""
TAG = _vsp.TAG
r""" Color mesh by tag value (component, subsurface, part, etc)"""
REASON = _vsp.REASON
r""" Color mesh by local edge length reason"""
CF_LAM_BLASIUS = _vsp.CF_LAM_BLASIUS
r""" Blasius laminar Cf equation"""
CF_LAM_BLASIUS_W_HEAT = _vsp.CF_LAM_BLASIUS_W_HEAT
r""" Blasius laminar Cf equation with heat (NOT IMPLEMENTED)"""
CF_TURB_EXPLICIT_FIT_SPALDING = _vsp.CF_TURB_EXPLICIT_FIT_SPALDING
r""" Explicit Fit of Spalding turbulent Cf equation"""
CF_TURB_EXPLICIT_FIT_SPALDING_CHI = _vsp.CF_TURB_EXPLICIT_FIT_SPALDING_CHI
r""" Explicit Fit of Spalding and Chi turbulent Cf equation"""
CF_TURB_EXPLICIT_FIT_SCHOENHERR = _vsp.CF_TURB_EXPLICIT_FIT_SCHOENHERR
r""" Explicit Fit of Schoenherr turbulent Cf equation"""
DO_NOT_USE_CF_TURB_IMPLICIT_KARMAN = _vsp.DO_NOT_USE_CF_TURB_IMPLICIT_KARMAN
r""" Implicit Karman turbulent Cf equation (DO NOT USE)"""
CF_TURB_IMPLICIT_SCHOENHERR = _vsp.CF_TURB_IMPLICIT_SCHOENHERR
r""" Implicit Schoenherr turbulent Cf equation"""
CF_TURB_IMPLICIT_KARMAN_SCHOENHERR = _vsp.CF_TURB_IMPLICIT_KARMAN_SCHOENHERR
r""" Implicit Karman-Schoenherr turbulent Cf equation"""
CF_TURB_POWER_LAW_BLASIUS = _vsp.CF_TURB_POWER_LAW_BLASIUS
r""" Power Law Blasius turbulent Cf equation"""
CF_TURB_POWER_LAW_PRANDTL_LOW_RE = _vsp.CF_TURB_POWER_LAW_PRANDTL_LOW_RE
r"""Power Law Prandtl Low Re turbulent Cf equation"""
CF_TURB_POWER_LAW_PRANDTL_MEDIUM_RE = _vsp.CF_TURB_POWER_LAW_PRANDTL_MEDIUM_RE
r""" Power Law Prandtl Medium Re turbulent Cf equation"""
CF_TURB_POWER_LAW_PRANDTL_HIGH_RE = _vsp.CF_TURB_POWER_LAW_PRANDTL_HIGH_RE
r""" Power Law Prandtl High Re turbulent Cf equation"""
CF_TURB_SCHLICHTING_COMPRESSIBLE = _vsp.CF_TURB_SCHLICHTING_COMPRESSIBLE
r""" Schlichting Compressible turbulent Cf equation"""
DO_NOT_USE_CF_TURB_SCHLICHTING_INCOMPRESSIBLE = _vsp.DO_NOT_USE_CF_TURB_SCHLICHTING_INCOMPRESSIBLE
r""" Schlichting Incompressible turbulent Cf equation (DO NOT USE)"""
DO_NOT_USE_CF_TURB_SCHLICHTING_PRANDTL = _vsp.DO_NOT_USE_CF_TURB_SCHLICHTING_PRANDTL
r""" Schlichting-Prandtl turbulent Cf equation (DO NOT USE)"""
DO_NOT_USE_CF_TURB_SCHULTZ_GRUNOW_HIGH_RE = _vsp.DO_NOT_USE_CF_TURB_SCHULTZ_GRUNOW_HIGH_RE
r""" Schultz-Grunow High Re turbulent Cf equation (DO NOT USE)"""
CF_TURB_SCHULTZ_GRUNOW_SCHOENHERR = _vsp.CF_TURB_SCHULTZ_GRUNOW_SCHOENHERR
r""" Schultz-Grunow Estimate of Schoenherr turbulent Cf equation."""
DO_NOT_USE_CF_TURB_WHITE_CHRISTOPH_COMPRESSIBLE = _vsp.DO_NOT_USE_CF_TURB_WHITE_CHRISTOPH_COMPRESSIBLE
r""" White-Christoph Compressible turbulent Cf equation (DO NOT USE)"""
CF_TURB_ROUGHNESS_SCHLICHTING_AVG = _vsp.CF_TURB_ROUGHNESS_SCHLICHTING_AVG
r""" Roughness Schlichting Avg turbulent Cf equation."""
DO_NOT_USE_CF_TURB_ROUGHNESS_SCHLICHTING_LOCAL = _vsp.DO_NOT_USE_CF_TURB_ROUGHNESS_SCHLICHTING_LOCAL
r""" Roughness Schlichting Local turbulent Cf equation (DO NOT USE)"""
DO_NOT_USE_CF_TURB_ROUGHNESS_WHITE = _vsp.DO_NOT_USE_CF_TURB_ROUGHNESS_WHITE
r""" Roughness White turbulent Cf equation (DO NOT USE)"""
CF_TURB_ROUGHNESS_SCHLICHTING_AVG_FLOW_CORRECTION = _vsp.CF_TURB_ROUGHNESS_SCHLICHTING_AVG_FLOW_CORRECTION
r""" Roughness Schlichting Avg Compressible turbulent Cf equation."""
CF_TURB_HEATTRANSFER_WHITE_CHRISTOPH = _vsp.CF_TURB_HEATTRANSFER_WHITE_CHRISTOPH
r""" Heat Transfer White-Christoph turbulent Cf equation."""
CHEVRON_NONE = _vsp.CHEVRON_NONE
r""" No chevron."""
CHEVRON_PARTIAL = _vsp.CHEVRON_PARTIAL
r""" One or more chevrons of limited extent."""
CHEVRON_FULL = _vsp.CHEVRON_FULL
r""" Full period of chevrons."""
CHEVRON_NUM_TYPES = _vsp.CHEVRON_NUM_TYPES
r""" Number of chevron types."""
CHEVRON_W01_SE = _vsp.CHEVRON_W01_SE
CHEVRON_W01_CW = _vsp.CHEVRON_W01_CW
CHEVRON_W01_NUM_MODES = _vsp.CHEVRON_W01_NUM_MODES
r""" Number of chevron W parameter mode types."""
COLLISION_OK = _vsp.COLLISION_OK
r""" No Error."""
COLLISION_INTERSECT_NO_SOLUTION = _vsp.COLLISION_INTERSECT_NO_SOLUTION
r""" Touching, no solution"""
COLLISION_CLEAR_NO_SOLUTION = _vsp.COLLISION_CLEAR_NO_SOLUTION
r""" Not touching, no solution"""
NO_FILE_TYPE = _vsp.NO_FILE_TYPE
r""" No export file type"""
COMP_GEOM_TXT_TYPE = _vsp.COMP_GEOM_TXT_TYPE
COMP_GEOM_CSV_TYPE = _vsp.COMP_GEOM_CSV_TYPE
DRAG_BUILD_TSV_TYPE_DEPRECATED = _vsp.DRAG_BUILD_TSV_TYPE_DEPRECATED
SLICE_TXT_TYPE = _vsp.SLICE_TXT_TYPE
MASS_PROP_TXT_TYPE = _vsp.MASS_PROP_TXT_TYPE
DEGEN_GEOM_CSV_TYPE = _vsp.DEGEN_GEOM_CSV_TYPE
DEGEN_GEOM_M_TYPE = _vsp.DEGEN_GEOM_M_TYPE
CFD_STL_TYPE = _vsp.CFD_STL_TYPE
CFD_POLY_TYPE = _vsp.CFD_POLY_TYPE
CFD_TRI_TYPE = _vsp.CFD_TRI_TYPE
CFD_OBJ_TYPE = _vsp.CFD_OBJ_TYPE
CFD_DAT_TYPE = _vsp.CFD_DAT_TYPE
CFD_KEY_TYPE = _vsp.CFD_KEY_TYPE
CFD_GMSH_TYPE = _vsp.CFD_GMSH_TYPE
CFD_SRF_TYPE_DEPRECATED = _vsp.CFD_SRF_TYPE_DEPRECATED
CFD_TKEY_TYPE = _vsp.CFD_TKEY_TYPE
PROJ_AREA_CSV_TYPE = _vsp.PROJ_AREA_CSV_TYPE
WAVE_DRAG_TXT_TYPE = _vsp.WAVE_DRAG_TXT_TYPE
VSPAERO_PANEL_TRI_TYPE = _vsp.VSPAERO_PANEL_TRI_TYPE
DRAG_BUILD_CSV_TYPE = _vsp.DRAG_BUILD_CSV_TYPE
CFD_FACET_TYPE = _vsp.CFD_FACET_TYPE
CFD_CURV_TYPE_DEPRECATED = _vsp.CFD_CURV_TYPE_DEPRECATED
CFD_PLOT3D_TYPE_DEPRECATED = _vsp.CFD_PLOT3D_TYPE_DEPRECATED
CFD_VSPGEOM_TYPE = _vsp.CFD_VSPGEOM_TYPE
VSPAERO_VSPGEOM_TYPE = _vsp.VSPAERO_VSPGEOM_TYPE
U_TRIM = _vsp.U_TRIM
r""" Trim by U coordinate"""
L_TRIM = _vsp.L_TRIM
r""" Trim by L coordinate"""
ETA_TRIM = _vsp.ETA_TRIM
r""" Trim by Eta coordinate"""
NUM_TRIM_TYPES = _vsp.NUM_TRIM_TYPES
r""" Number of conformal component trim types"""
DELIM_COMMA = _vsp.DELIM_COMMA
r""" Comma delimiter"""
DELIM_USCORE = _vsp.DELIM_USCORE
r""" Underscore delimiter"""
DELIM_SPACE = _vsp.DELIM_SPACE
r""" Space delimiter"""
DELIM_NONE = _vsp.DELIM_NONE
r""" No delimiter"""
DELIM_NUM_TYPES = _vsp.DELIM_NUM_TYPES
r""" Number of delimiter types"""
DEPTH_FRONT = _vsp.DEPTH_FRONT
r""" Set 3D background before model"""
DEPTH_REAR = _vsp.DEPTH_REAR
r""" Set 3D background behind model"""
DEPTH_FREE = _vsp.DEPTH_FREE
r""" Set 3D background at specified location"""
NUM_DEPTH_TYPE = _vsp.NUM_DEPTH_TYPE
r""" Number of depth types"""
SET_3D = _vsp.SET_3D
r""" 3D DXF export (default)"""
SET_2D = _vsp.SET_2D
r""" 2D DXF export"""
X_DIR = _vsp.X_DIR
r""" X direction"""
Y_DIR = _vsp.Y_DIR
Z_DIR = _vsp.Z_DIR
ALL_DIR = _vsp.ALL_DIR
DISPLAY_BEZIER = _vsp.DISPLAY_BEZIER
r""" Display the normal Bezier surface (default)"""
DISPLAY_DEGEN_SURF = _vsp.DISPLAY_DEGEN_SURF
r""" Display as surface Degen Geom"""
DISPLAY_DEGEN_PLATE = _vsp.DISPLAY_DEGEN_PLATE
r""" Display as plate Degen Geom"""
DISPLAY_DEGEN_CAMBER = _vsp.DISPLAY_DEGEN_CAMBER
r""" Display as camber Degen Geom"""
GEOM_DRAW_WIRE = _vsp.GEOM_DRAW_WIRE
r""" Draw the wireframe mesh (see through)"""
GEOM_DRAW_HIDDEN = _vsp.GEOM_DRAW_HIDDEN
r""" Draw the hidden mesh"""
GEOM_DRAW_SHADE = _vsp.GEOM_DRAW_SHADE
r""" Draw the shaded mesh"""
GEOM_DRAW_TEXTURE = _vsp.GEOM_DRAW_TEXTURE
r""" Draw the textured mesh"""
GEOM_DRAW_NONE = _vsp.GEOM_DRAW_NONE
r""" Do not draw anything"""
ENGINE_GEOM_NONE = _vsp.ENGINE_GEOM_NONE
r""" Component is not an integrated flowpath component."""
ENGINE_GEOM_INLET = _vsp.ENGINE_GEOM_INLET
r""" Component represents integrated flowpath inlet."""
ENGINE_GEOM_INLET_OUTLET = _vsp.ENGINE_GEOM_INLET_OUTLET
r""" Component represents integrated flowpath inlet and outlet."""
ENGINE_GEOM_OUTLET = _vsp.ENGINE_GEOM_OUTLET
r""" Component represents integrated flowpath outlet."""
ENGINE_GEOM_IO_NUM_TYPES = _vsp.ENGINE_GEOM_IO_NUM_TYPES
r""" Number of integrated flowpath component types."""
ENGINE_GEOM_FLOWTHROUGH = _vsp.ENGINE_GEOM_FLOWTHROUGH
r""" Component is modeled as flowthrough engine."""
ENGINE_GEOM_TO_LIP = _vsp.ENGINE_GEOM_TO_LIP
r""" Component is modeled to the lip."""
ENGINE_GEOM_FLOWPATH = _vsp.ENGINE_GEOM_FLOWPATH
r""" Component flowpath is modeled."""
ENGINE_GEOM_TO_FACE = _vsp.ENGINE_GEOM_TO_FACE
r""" Component is modeled to face."""
ENGINE_GEOM_NUM_TYPES = _vsp.ENGINE_GEOM_NUM_TYPES
r""" Number of integrated flowpath modeling types."""
ENGINE_LOC_INDEX = _vsp.ENGINE_LOC_INDEX
r""" Integrated flowpath key point identified by XSec index."""
ENGINE_LOC_U = _vsp.ENGINE_LOC_U
r""" Integrated flowpath key point identified by U parameter."""
ENGINE_LOC_INLET_LIP = _vsp.ENGINE_LOC_INLET_LIP
r""" Integrated flowpath key point is inlet lip."""
ENGINE_LOC_INLET_FACE = _vsp.ENGINE_LOC_INLET_FACE
r""" Integrated flowpath key point is inlet face."""
ENGINE_LOC_OUTLET_LIP = _vsp.ENGINE_LOC_OUTLET_LIP
r""" Integrated flowpath key point is outlet lip."""
ENGINE_LOC_OUTLET_FACE = _vsp.ENGINE_LOC_OUTLET_FACE
r""" Integrated flowpath key point is outlet face."""
ENGINE_LOC_NUM = _vsp.ENGINE_LOC_NUM
r""" Number of integrated flowpath key point locations."""
ENGINE_MODE_FLOWTHROUGH = _vsp.ENGINE_MODE_FLOWTHROUGH
r""" Represent integrated flowpath as flowthrough engine."""
ENGINE_MODE_FLOWTHROUGH_NEG = _vsp.ENGINE_MODE_FLOWTHROUGH_NEG
r""" Represent integrated flowpath as flowthrough engine with negative flowpath."""
ENGINE_MODE_TO_LIP = _vsp.ENGINE_MODE_TO_LIP
r""" Represent integrated flowpath to the lip."""
ENGINE_MODE_TO_FACE = _vsp.ENGINE_MODE_TO_FACE
r""" Represent integrated flowpath to the face."""
ENGINE_MODE_TO_FACE_NEG = _vsp.ENGINE_MODE_TO_FACE_NEG
r""" Represent integrated flowpath to the face with negative flowpath to the face."""
ENGINE_MODE_EXTEND = _vsp.ENGINE_MODE_EXTEND
r""" Represent integrated flowpath with farfield extensions."""
ENGINE_MODE_NUM_TYPES = _vsp.ENGINE_MODE_NUM_TYPES
r""" Number of integrated flowpath representations."""
VSP_OK = _vsp.VSP_OK
r""" No error"""
VSP_INVALID_PTR = _vsp.VSP_INVALID_PTR
r""" Invalid pointer error"""
VSP_INVALID_TYPE = _vsp.VSP_INVALID_TYPE
r""" Invalid type error"""
VSP_CANT_FIND_TYPE = _vsp.VSP_CANT_FIND_TYPE
r""" Can't find type error"""
VSP_CANT_FIND_PARM = _vsp.VSP_CANT_FIND_PARM
r""" Can't find parm error"""
VSP_CANT_FIND_NAME = _vsp.VSP_CANT_FIND_NAME
r""" Can't find name error"""
VSP_INVALID_GEOM_ID = _vsp.VSP_INVALID_GEOM_ID
r""" Invalid Geom ID error"""
VSP_FILE_DOES_NOT_EXIST = _vsp.VSP_FILE_DOES_NOT_EXIST
r""" File does not exist error"""
VSP_FILE_WRITE_FAILURE = _vsp.VSP_FILE_WRITE_FAILURE
r""" File write failure error"""
VSP_FILE_READ_FAILURE = _vsp.VSP_FILE_READ_FAILURE
r""" File read failure error"""
VSP_WRONG_GEOM_TYPE = _vsp.VSP_WRONG_GEOM_TYPE
r""" Wrong Geom type error"""
VSP_WRONG_XSEC_TYPE = _vsp.VSP_WRONG_XSEC_TYPE
r""" Wrong XSec type error"""
VSP_WRONG_FILE_TYPE = _vsp.VSP_WRONG_FILE_TYPE
r""" Wrong file type error"""
VSP_INDEX_OUT_RANGE = _vsp.VSP_INDEX_OUT_RANGE
r""" Index out of range error"""
VSP_INVALID_XSEC_ID = _vsp.VSP_INVALID_XSEC_ID
r""" Invalid XSec ID error"""
VSP_INVALID_ID = _vsp.VSP_INVALID_ID
r""" Invalid ID error"""
VSP_CANT_SET_NOT_EQ_PARM = _vsp.VSP_CANT_SET_NOT_EQ_PARM
r""" Can't set NotEqParm error"""
VSP_AMBIGUOUS_SUBSURF = _vsp.VSP_AMBIGUOUS_SUBSURF
r""" Ambiguous flow-through sub-surface error"""
VSP_INVALID_VARPRESET_SETNAME = _vsp.VSP_INVALID_VARPRESET_SETNAME
r""" Invalid Variable Preset set name error"""
VSP_INVALID_VARPRESET_GROUPNAME = _vsp.VSP_INVALID_VARPRESET_GROUPNAME
r""" Invalid Variable Preset group name error"""
VSP_CONFORMAL_PARENT_UNSUPPORTED = _vsp.VSP_CONFORMAL_PARENT_UNSUPPORTED
r""" Unsupported Conformal Geom parent error"""
VSP_UNEXPECTED_RESET_REMAP_ID = _vsp.VSP_UNEXPECTED_RESET_REMAP_ID
r""" Unexpected reset remap ID error"""
VSP_INVALID_INPUT_VAL = _vsp.VSP_INVALID_INPUT_VAL
r""" Invalid input value error"""
VSP_INVALID_CF_EQN = _vsp.VSP_INVALID_CF_EQN
r""" Invalid friction coefficient equation error"""
VSP_INVALID_DRIVERS = _vsp.VSP_INVALID_DRIVERS
r""" Invalid drivers for driver group"""
VSP_ADV_LINK_BUILD_FAIL = _vsp.VSP_ADV_LINK_BUILD_FAIL
r""" Advanced link build failure"""
VSP_DEPRECATED = _vsp.VSP_DEPRECATED
r""" This capability has been deprecated and is not longer supported"""
VSP_LINK_LOOP_DETECTED = _vsp.VSP_LINK_LOOP_DETECTED
r""" A parameter link loop was detected and stopped"""
VSP_DUPLICATE_NAME = _vsp.VSP_DUPLICATE_NAME
r""" A duplicate name has been provided"""
VSP_GUI_DEVICE_DEACTIVATED = _vsp.VSP_GUI_DEVICE_DEACTIVATED
r""" A deactivated GUI device was touched"""
VSP_NUM_ERROR_CODE = _vsp.VSP_NUM_ERROR_CODE
r""" Total number of VSP error codes"""
EXCRESCENCE_COUNT = _vsp.EXCRESCENCE_COUNT
r""" Drag counts excressence type"""
EXCRESCENCE_CD = _vsp.EXCRESCENCE_CD
r""" Drag coefficient excressence type"""
EXCRESCENCE_PERCENT_GEOM = _vsp.EXCRESCENCE_PERCENT_GEOM
r""" Percent of parent Geom drag coefficient excressence type"""
EXCRESCENCE_MARGIN = _vsp.EXCRESCENCE_MARGIN
r""" Percent margin excressence type"""
EXCRESCENCE_DRAGAREA = _vsp.EXCRESCENCE_DRAGAREA
r""" Drag area (D/q) excressence type"""
EXPORT_FELISA = _vsp.EXPORT_FELISA
r""" FELISA export type (NOT IMPLEMENTED)"""
EXPORT_XSEC = _vsp.EXPORT_XSEC
r""" XSec (*.hrm) export type"""
EXPORT_STL = _vsp.EXPORT_STL
r""" Stereolith (*.stl) export type"""
EXPORT_AWAVE = _vsp.EXPORT_AWAVE
r""" AWAVE export type (NOT IMPLEMENTED)"""
EXPORT_NASCART = _vsp.EXPORT_NASCART
r""" NASCART (*.dat) export type"""
EXPORT_POVRAY = _vsp.EXPORT_POVRAY
r""" POVRAY (*.pov) export type"""
EXPORT_CART3D = _vsp.EXPORT_CART3D
r""" Cart3D (*.tri) export type"""
EXPORT_VSPGEOM = _vsp.EXPORT_VSPGEOM
r""" VSPGeom (*.vspgeom) export type"""
EXPORT_VORXSEC = _vsp.EXPORT_VORXSEC
r""" VORXSEC  export type (NOT IMPLEMENTED)"""
EXPORT_XSECGEOM = _vsp.EXPORT_XSECGEOM
r""" XSECGEOM export type (NOT IMPLEMENTED)"""
EXPORT_GMSH = _vsp.EXPORT_GMSH
r""" Gmsh (*.msh) export type"""
EXPORT_X3D = _vsp.EXPORT_X3D
r""" X3D (*.x3d) export type"""
EXPORT_STEP = _vsp.EXPORT_STEP
r""" STEP (*.stp) export type"""
EXPORT_PLOT3D = _vsp.EXPORT_PLOT3D
r""" PLOT3D (*.p3d) export type"""
EXPORT_IGES = _vsp.EXPORT_IGES
r""" IGES (*.igs) export type"""
EXPORT_BEM = _vsp.EXPORT_BEM
r""" Blade Element (*.bem) export type"""
EXPORT_DXF = _vsp.EXPORT_DXF
r""" AutoCAD (*.dxf) export type"""
EXPORT_FACET = _vsp.EXPORT_FACET
r""" Xpatch (*.facet) export type"""
EXPORT_SVG = _vsp.EXPORT_SVG
r""" SVG (*.svg) export type"""
EXPORT_PMARC = _vsp.EXPORT_PMARC
r""" PMARC 12 (*.pmin) export type"""
EXPORT_OBJ = _vsp.EXPORT_OBJ
r""" OBJ (*.obj) export type"""
EXPORT_SELIG_AIRFOIL = _vsp.EXPORT_SELIG_AIRFOIL
r""" Airfoil points (*.dat) export type"""
EXPORT_BEZIER_AIRFOIL = _vsp.EXPORT_BEZIER_AIRFOIL
r""" Airfoil curves (*.bz) export type"""
EXPORT_IGES_STRUCTURE = _vsp.EXPORT_IGES_STRUCTURE
r""" IGES structure (*.igs) export type"""
EXPORT_STEP_STRUCTURE = _vsp.EXPORT_STEP_STRUCTURE
r""" STEP structure (*.stp) export type"""
FEA_BC_STRUCTURE = _vsp.FEA_BC_STRUCTURE
r""" FEA boundary condition assigned to structure."""
FEA_BC_PART = _vsp.FEA_BC_PART
r""" FEA boundary condition assigned to part."""
FEA_BC_SUBSURF = _vsp.FEA_BC_SUBSURF
r""" FEA boundary condition assigned to subsurface."""
FEA_NUM_BC_TYPES = _vsp.FEA_NUM_BC_TYPES
r""" Number of FEA boundary condition definition types."""
FEA_BCM_USER = _vsp.FEA_BCM_USER
r""" FEA boundary condition constraints user defined."""
FEA_BCM_ALL = _vsp.FEA_BCM_ALL
r""" FEA boundary condition constrains all DOF."""
FEA_BCM_PIN = _vsp.FEA_BCM_PIN
r""" FEA boundary condition pin constraints."""
FEA_BCM_SYMM = _vsp.FEA_BCM_SYMM
r""" FEA boundary condition symmetrical constraints."""
FEA_BCM_ASYMM = _vsp.FEA_BCM_ASYMM
r""" FEA boundary condition antisymmetrical constraints."""
FEA_NUM_BCM_MODES = _vsp.FEA_NUM_BCM_MODES
r""" Number of FEA boundary condition constraint types."""
FEA_XSEC_GENERAL = _vsp.FEA_XSEC_GENERAL
r""" General XSec type"""
FEA_XSEC_CIRC = _vsp.FEA_XSEC_CIRC
r""" Circle XSec type"""
FEA_XSEC_PIPE = _vsp.FEA_XSEC_PIPE
r""" Pipe XSec type"""
FEA_XSEC_I = _vsp.FEA_XSEC_I
r""" I XSec type"""
FEA_XSEC_RECT = _vsp.FEA_XSEC_RECT
r""" Rectangle XSec type"""
FEA_XSEC_BOX = _vsp.FEA_XSEC_BOX
r""" Box XSec type"""
FEA_MASS_FILE_NAME = _vsp.FEA_MASS_FILE_NAME
r""" FEA Mesh mass export type"""
FEA_NASTRAN_FILE_NAME = _vsp.FEA_NASTRAN_FILE_NAME
r""" FEA Mesh NASTRAN export type"""
FEA_NKEY_FILE_NAME = _vsp.FEA_NKEY_FILE_NAME
r""" FEA Mesh NKey export type"""
FEA_CALCULIX_FILE_NAME = _vsp.FEA_CALCULIX_FILE_NAME
r""" FEA Mesh Calculix export type"""
FEA_STL_FILE_NAME = _vsp.FEA_STL_FILE_NAME
r""" FEA Mesh STL export type"""
FEA_GMSH_FILE_NAME = _vsp.FEA_GMSH_FILE_NAME
r""" FEA Mesh GMSH export type"""
FEA_SRF_FILE_NAME = _vsp.FEA_SRF_FILE_NAME
r""" FEA Mesh SRF export type"""
FEA_CURV_FILE_NAME = _vsp.FEA_CURV_FILE_NAME
r""" FEA Mesh CURV export type"""
FEA_PLOT3D_FILE_NAME = _vsp.FEA_PLOT3D_FILE_NAME
r""" FEA Mesh PLOT3D export type"""
FEA_IGES_FILE_NAME = _vsp.FEA_IGES_FILE_NAME
r""" FEA Mesh trimmed IGES export type"""
FEA_STEP_FILE_NAME = _vsp.FEA_STEP_FILE_NAME
r""" FEA Mesh trimmed STEP export type"""
FEA_NUM_FILE_NAMES = _vsp.FEA_NUM_FILE_NAMES
r""" Number of FEA Mesh export type."""
FEA_FIX_PT_ON_BODY = _vsp.FEA_FIX_PT_ON_BODY
r""" On body fixed point type"""
FEA_FIX_PT_GLOBAL_XYZ = _vsp.FEA_FIX_PT_GLOBAL_XYZ
r""" Global XYZ off body fixed point type"""
FEA_FIX_PT_DELTA_XYZ = _vsp.FEA_FIX_PT_DELTA_XYZ
r""" Delta XYZ off body fixed point type"""
FEA_FIX_PT_DELTA_UVN = _vsp.FEA_FIX_PT_DELTA_UVN
r""" Delta UVN off body fixed point type"""
FEA_FIX_PT_GEOM_ORIGIN = _vsp.FEA_FIX_PT_GEOM_ORIGIN
r""" Geom origin off body fixed point type"""
FEA_FIX_PT_GEOM_CG = _vsp.FEA_FIX_PT_GEOM_CG
r""" Geom CG off body fixed point type"""
FEA_NUM_FIX_PT_TYPES = _vsp.FEA_NUM_FIX_PT_TYPES
r""" Number of off body fixed point types"""
FEA_ISOTROPIC = _vsp.FEA_ISOTROPIC
r""" Isotropic material"""
FEA_ENG_ORTHO = _vsp.FEA_ENG_ORTHO
r""" Orthotropic material in engineering parameters"""
FEA_ENG_ORTHO_TRANS_ISO = _vsp.FEA_ENG_ORTHO_TRANS_ISO
r""" Orthotropic material with transverse isotropy assumed in engineering parameters"""
FEA_LAMINATE = _vsp.FEA_LAMINATE
r""" Laminate buildup material"""
FEA_NUM_MAT_TYPES = _vsp.FEA_NUM_MAT_TYPES
r""" Number of FEA material types"""
FEA_ORIENT_GLOBAL_X = _vsp.FEA_ORIENT_GLOBAL_X
r""" FEA Global X material orientation"""
FEA_ORIENT_GLOBAL_Y = _vsp.FEA_ORIENT_GLOBAL_Y
r""" FEA Global Y material orientation"""
FEA_ORIENT_GLOBAL_Z = _vsp.FEA_ORIENT_GLOBAL_Z
r""" FEA Global Z material orientation"""
FEA_ORIENT_COMP_X = _vsp.FEA_ORIENT_COMP_X
r""" FEA Comp X material orientation"""
FEA_ORIENT_COMP_Y = _vsp.FEA_ORIENT_COMP_Y
r""" FEA Comp Y material orientation"""
FEA_ORIENT_COMP_Z = _vsp.FEA_ORIENT_COMP_Z
r""" FEA Comp Z material orientation"""
FEA_ORIENT_PART_U = _vsp.FEA_ORIENT_PART_U
r""" FEA Part U material orientation"""
FEA_ORIENT_PART_V = _vsp.FEA_ORIENT_PART_V
r""" FEA Part V material orientation"""
FEA_ORIENT_OML_U = _vsp.FEA_ORIENT_OML_U
r""" FEA OML U material orientation"""
FEA_ORIENT_OML_V = _vsp.FEA_ORIENT_OML_V
r""" FEA OML V material orientation"""
FEA_ORIENT_OML_R = _vsp.FEA_ORIENT_OML_R
r""" FEA OML R material orientation"""
FEA_ORIENT_OML_S = _vsp.FEA_ORIENT_OML_S
r""" FEA OML S material orientation"""
FEA_ORIENT_OML_T = _vsp.FEA_ORIENT_OML_T
r""" FEA OML T material orientation"""
FEA_NUM_ORIENT_TYPES = _vsp.FEA_NUM_ORIENT_TYPES
r""" Number of FEA material orientation types"""
FEA_DEPRECATED = _vsp.FEA_DEPRECATED
r""" Flag for deprecated element type option"""
FEA_SHELL = _vsp.FEA_SHELL
r""" Shell (tris) FEA element type"""
FEA_BEAM = _vsp.FEA_BEAM
r""" Beam FEA element type"""
FEA_SHELL_AND_BEAM = _vsp.FEA_SHELL_AND_BEAM
r""" Both Shell and Beam FEA element types"""
FEA_NO_ELEMENTS = _vsp.FEA_NO_ELEMENTS
r""" FEA part with no elements"""
FEA_NUM_ELEMENT_TYPES = _vsp.FEA_NUM_ELEMENT_TYPES
r""" Number of FEA element type choices"""
FEA_KEEP = _vsp.FEA_KEEP
r""" Keep shell elements"""
FEA_DELETE = _vsp.FEA_DELETE
r""" Delete shell elements"""
FEA_NUM_SHELL_TREATMENT_TYPES = _vsp.FEA_NUM_SHELL_TREATMENT_TYPES
r""" Number of FEA subsurface treatment choices"""
FEA_SLICE = _vsp.FEA_SLICE
r""" Slice FEA Part type"""
FEA_RIB = _vsp.FEA_RIB
r""" Rib FEA Part type"""
FEA_SPAR = _vsp.FEA_SPAR
r""" Spar FEA Part type"""
FEA_FIX_POINT = _vsp.FEA_FIX_POINT
r""" Fixed Point FEA Part type"""
FEA_DOME = _vsp.FEA_DOME
r""" Dome FEA Part type"""
FEA_RIB_ARRAY = _vsp.FEA_RIB_ARRAY
r""" Rib array FEA Part type"""
FEA_SLICE_ARRAY = _vsp.FEA_SLICE_ARRAY
r""" Slice array FEA Part type"""
FEA_SKIN = _vsp.FEA_SKIN
r""" Skin FEA Part type"""
FEA_TRIM = _vsp.FEA_TRIM
r""" Trim FEA Part type"""
FEA_NUM_TYPES = _vsp.FEA_NUM_TYPES
r""" Number of FEA Part types"""
XY_BODY = _vsp.XY_BODY
r""" Slice is parallel to parent Geom body XY plane"""
YZ_BODY = _vsp.YZ_BODY
r""" Slice is parallel to parent Geom body YZ plane"""
XZ_BODY = _vsp.XZ_BODY
r""" Slice is parallel to parent Geom body XZ plane"""
XY_ABS = _vsp.XY_ABS
r""" Slice is parallel to absolute XY plane"""
YZ_ABS = _vsp.YZ_ABS
r""" Slice is parallel to absolute YZ plane"""
XZ_ABS = _vsp.XZ_ABS
r""" Slice is parallel to absolute XZ plane"""
SPINE_NORMAL = _vsp.SPINE_NORMAL
r""" Slice is perpendicular to thespine of the parent Geom"""
SI_UNIT = _vsp.SI_UNIT
r""" FEA Files output in (m, kg)"""
CGS_UNIT = _vsp.CGS_UNIT
r""" FEA Files output in (cm, g)"""
MPA_UNIT = _vsp.MPA_UNIT
r""" FEA Files output in (mm, tonne)"""
BFT_UNIT = _vsp.BFT_UNIT
r""" FEA Files output in (ft, slug)"""
BIN_UNIT = _vsp.BIN_UNIT
r""" FEA Files output in (in, lbf*sec^2/in)"""
NO_NORMAL = _vsp.NO_NORMAL
r""" FEA Rib or Rib Array has no set perpendicular edge"""
LE_NORMAL = _vsp.LE_NORMAL
r""" FEA Rib or Rib Array is set perpendicular to the leading edge"""
TE_NORMAL = _vsp.TE_NORMAL
r""" FEA Rib or Rib Array is set perpendicular to the trailing edge"""
SPAR_NORMAL = _vsp.SPAR_NORMAL
r""" FEA Rib or Rib Array is set perpendicular to an FEA Spar"""
FF_B_MANUAL = _vsp.FF_B_MANUAL
r""" Manual FF equation"""
FF_B_SCHEMENSKY_FUSE = _vsp.FF_B_SCHEMENSKY_FUSE
r""" Schemensky Fuselage FF equation"""
FF_B_SCHEMENSKY_NACELLE = _vsp.FF_B_SCHEMENSKY_NACELLE
r""" Schemensky Nacelle FF equation"""
FF_B_HOERNER_STREAMBODY = _vsp.FF_B_HOERNER_STREAMBODY
r""" Hoerner Streamlined Body FF equation"""
FF_B_TORENBEEK = _vsp.FF_B_TORENBEEK
r""" Torenbeek FF equation"""
FF_B_SHEVELL = _vsp.FF_B_SHEVELL
r""" Shevell FF equation"""
FF_B_COVERT = _vsp.FF_B_COVERT
r""" Covert FF equation"""
FF_B_JENKINSON_FUSE = _vsp.FF_B_JENKINSON_FUSE
r""" Jenkinson Fuselage FF equation"""
FF_B_JENKINSON_WING_NACELLE = _vsp.FF_B_JENKINSON_WING_NACELLE
r""" Jenkinson Wing Nacelle FF equation"""
FF_B_JENKINSON_AFT_FUSE_NACELLE = _vsp.FF_B_JENKINSON_AFT_FUSE_NACELLE
r""" Jenkinson Aft Fuselage Nacelle FF equation"""
FF_W_MANUAL = _vsp.FF_W_MANUAL
r""" Manual FF equation"""
FF_W_EDET_CONV = _vsp.FF_W_EDET_CONV
r""" EDET Conventional Airfoil FF equation"""
FF_W_EDET_ADV = _vsp.FF_W_EDET_ADV
r""" EDET Advanced Airfoil FF equation"""
FF_W_HOERNER = _vsp.FF_W_HOERNER
r""" Hoerner FF equation"""
FF_W_COVERT = _vsp.FF_W_COVERT
r""" Covert FF equation"""
FF_W_SHEVELL = _vsp.FF_W_SHEVELL
r""" Shevell FF equation"""
FF_W_KROO = _vsp.FF_W_KROO
r""" Kroo FF equation"""
FF_W_TORENBEEK = _vsp.FF_W_TORENBEEK
r""" Torenbeek FF equation"""
FF_W_DATCOM = _vsp.FF_W_DATCOM
r""" DATCOM FF equation"""
FF_W_SCHEMENSKY_6_SERIES_AF = _vsp.FF_W_SCHEMENSKY_6_SERIES_AF
r""" Schemensky 6 Series Airfoil FF equation"""
FF_W_SCHEMENSKY_4_SERIES_AF = _vsp.FF_W_SCHEMENSKY_4_SERIES_AF
r""" Schemensky 4 Series Airfoil FF equation"""
FF_W_JENKINSON_WING = _vsp.FF_W_JENKINSON_WING
r""" Jenkinson Wing FF equation"""
FF_W_JENKINSON_TAIL = _vsp.FF_W_JENKINSON_TAIL
r""" Jenkinson Tail FF equation"""
FF_W_SCHEMENSKY_SUPERCRITICAL_AF = _vsp.FF_W_SCHEMENSKY_SUPERCRITICAL_AF
r""" Schemensky Supercritical Airfoil FF equation"""
PD_UNITS_IMPERIAL = _vsp.PD_UNITS_IMPERIAL
r""" Imperial unit system"""
PD_UNITS_METRIC = _vsp.PD_UNITS_METRIC
r""" Metric unit system"""
OPEN = _vsp.OPEN
r""" Browse files that already exist"""
SAVE = _vsp.SAVE
r""" Browse file system and enter file name"""
NUM_FILE_CHOOSER_MODES = _vsp.NUM_FILE_CHOOSER_MODES
r""" Number of file chooser modes"""
FC_OPENVSP = _vsp.FC_OPENVSP
r""" OpenVSP's own file chooser with directory preferences."""
FC_NATIVE = _vsp.FC_NATIVE
r""" Operating system's native file chooser"""
NUM_FILE_CHOOSER_TYPES = _vsp.NUM_FILE_CHOOSER_TYPES
r""" Number of file chooser types"""
GDEV_TAB = _vsp.GDEV_TAB
r""" Custom GUI Tab"""
GDEV_SCROLL_TAB = _vsp.GDEV_SCROLL_TAB
r""" Custom GUI Fl_Scroll and Tab"""
GDEV_GROUP = _vsp.GDEV_GROUP
r""" Custom GUI Group"""
GDEV_PARM_BUTTON = _vsp.GDEV_PARM_BUTTON
r""" Custom GUI ParmButton"""
GDEV_INPUT = _vsp.GDEV_INPUT
r""" Custom GUI Input"""
GDEV_OUTPUT = _vsp.GDEV_OUTPUT
r""" Custom GUI Output"""
GDEV_SLIDER = _vsp.GDEV_SLIDER
r""" Custom GUI Slider"""
GDEV_SLIDER_ADJ_RANGE = _vsp.GDEV_SLIDER_ADJ_RANGE
r""" Custom GUI SliderAdjRangeInput"""
GDEV_CHECK_BUTTON = _vsp.GDEV_CHECK_BUTTON
r""" Custom GUI CheckButton"""
GDEV_CHECK_BUTTON_BIT = _vsp.GDEV_CHECK_BUTTON_BIT
r""" Custom GUI CheckButtonBit"""
GDEV_RADIO_BUTTON = _vsp.GDEV_RADIO_BUTTON
r""" Custom GUI RadioButton"""
GDEV_TOGGLE_BUTTON = _vsp.GDEV_TOGGLE_BUTTON
r""" Custom GUI ToggleButton"""
GDEV_TOGGLE_RADIO_GROUP = _vsp.GDEV_TOGGLE_RADIO_GROUP
r""" Custom GUI ToggleRadioGroup (NOT IMPLEMENTED)"""
GDEV_TRIGGER_BUTTON = _vsp.GDEV_TRIGGER_BUTTON
r""" Custom GUI TriggerButton"""
GDEV_COUNTER = _vsp.GDEV_COUNTER
r""" Custom GUI Counter"""
GDEV_CHOICE = _vsp.GDEV_CHOICE
r""" Custom GUI Choice"""
GDEV_ADD_CHOICE_ITEM = _vsp.GDEV_ADD_CHOICE_ITEM
r""" Add item to custom GUI Choice"""
GDEV_SLIDER_INPUT = _vsp.GDEV_SLIDER_INPUT
r""" Custom GUI SliderInput"""
GDEV_SLIDER_ADJ_RANGE_INPUT = _vsp.GDEV_SLIDER_ADJ_RANGE_INPUT
r""" Custom GUI SliderAdjRangeInput"""
GDEV_SLIDER_ADJ_RANGE_TWO_INPUT = _vsp.GDEV_SLIDER_ADJ_RANGE_TWO_INPUT
r""" Custom GUI SliderAdjRangeInput with two inputs (NOT IMPLEMENTED)"""
GDEV_FRACT_PARM_SLIDER = _vsp.GDEV_FRACT_PARM_SLIDER
r""" Custom GUI FractParmSlider"""
GDEV_STRING_INPUT = _vsp.GDEV_STRING_INPUT
r""" Custom GUI StringInput"""
GDEV_INDEX_SELECTOR = _vsp.GDEV_INDEX_SELECTOR
r""" Custom GUI IndexSelector"""
GDEV_COLOR_PICKER = _vsp.GDEV_COLOR_PICKER
r""" Custom GUI ColorPicker"""
GDEV_YGAP = _vsp.GDEV_YGAP
r""" Custom GUI Y gap"""
GDEV_DIVIDER_BOX = _vsp.GDEV_DIVIDER_BOX
r""" Custom GUI divider box"""
GDEV_BEGIN_SAME_LINE = _vsp.GDEV_BEGIN_SAME_LINE
r""" Set begin same line flag for custom GUI"""
GDEV_END_SAME_LINE = _vsp.GDEV_END_SAME_LINE
r""" Set end same line flag for custom GUI"""
GDEV_FORCE_WIDTH = _vsp.GDEV_FORCE_WIDTH
r""" Set forced width for custom GUI"""
GDEV_SET_FORMAT = _vsp.GDEV_SET_FORMAT
r""" Set format label for custom GUI"""
NUM_GDEV_TYPES = _vsp.NUM_GDEV_TYPES
r""" Number of GDEV types"""
ALL_GDEV_TYPES = _vsp.ALL_GDEV_TYPES
r""" Flag for all GDEV types"""
MALE = _vsp.MALE
r""" Male Human component"""
FEMALE = _vsp.FEMALE
r""" Female Human component"""
POD_GEOM_SCREEN = _vsp.POD_GEOM_SCREEN
r""" Pod geom screen"""
FUSELAGE_GEOM_SCREEN = _vsp.FUSELAGE_GEOM_SCREEN
r""" Fuselage geom screen"""
MS_WING_GEOM_SCREEN = _vsp.MS_WING_GEOM_SCREEN
r""" Wing geom screen"""
BLANK_GEOM_SCREEN = _vsp.BLANK_GEOM_SCREEN
r""" Blank geom screen"""
MESH_GEOM_SCREEN = _vsp.MESH_GEOM_SCREEN
r""" Mesh geom screen"""
STACK_GEOM_SCREEN = _vsp.STACK_GEOM_SCREEN
r""" Stack geom screen"""
CUSTOM_GEOM_SCREEN = _vsp.CUSTOM_GEOM_SCREEN
r""" Custom geom screen"""
PT_CLOUD_GEOM_SCREEN = _vsp.PT_CLOUD_GEOM_SCREEN
r""" Point cloud geom screen"""
PROP_GEOM_SCREEN = _vsp.PROP_GEOM_SCREEN
r""" Propeller geom screen"""
HINGE_GEOM_SCREEN = _vsp.HINGE_GEOM_SCREEN
r""" Hinge geom screen"""
MULT_GEOM_SCREEN = _vsp.MULT_GEOM_SCREEN
r""" Multiple geom screen"""
CONFORMAL_SCREEN = _vsp.CONFORMAL_SCREEN
r""" Conformal geom screen"""
ELLIPSOID_GEOM_SCREEN = _vsp.ELLIPSOID_GEOM_SCREEN
r""" Ellipsoid geom screen"""
BOR_GEOM_SCREEN = _vsp.BOR_GEOM_SCREEN
r""" Body of revolution geom screen"""
WIRE_FRAME_GEOM_SCREEN = _vsp.WIRE_FRAME_GEOM_SCREEN
r""" Wireframe geom screen"""
HUMAN_GEOM_SCREEN = _vsp.HUMAN_GEOM_SCREEN
r""" Human geom screen"""
NUM_GEOM_SCREENS = _vsp.NUM_GEOM_SCREENS
r""" Number of geom screens"""
ALL_GEOM_SCREENS = _vsp.ALL_GEOM_SCREENS
r""" All geom screens"""
VSP_ADV_LINK_SCREEN = _vsp.VSP_ADV_LINK_SCREEN
r""" Advanced linking screen"""
VSP_ADV_LINK_VAR_RENAME_SCREEN = _vsp.VSP_ADV_LINK_VAR_RENAME_SCREEN
r""" Advanced link variable rename screen"""
VSP_AERO_STRUCT_SCREEN = _vsp.VSP_AERO_STRUCT_SCREEN
r""" Aero / structural analysis screen"""
VSP_AIRFOIL_CURVES_EXPORT_SCREEN = _vsp.VSP_AIRFOIL_CURVES_EXPORT_SCREEN
r""" Airfoil curves export screen"""
VSP_AIRFOIL_POINTS_EXPORT_SCREEN = _vsp.VSP_AIRFOIL_POINTS_EXPORT_SCREEN
r""" Airfoil points screen"""
VSP_BACKGROUND_SCREEN = _vsp.VSP_BACKGROUND_SCREEN
r""" Background control screen"""
VSP_BACKGROUND3D_SCREEN = _vsp.VSP_BACKGROUND3D_SCREEN
r""" Background3D control screen"""
VSP_BACKGROUND3D_PREVIEW_SCREEN = _vsp.VSP_BACKGROUND3D_PREVIEW_SCREEN
r""" Background3D preview screen"""
VSP_BEM_OPTIONS_SCREEN = _vsp.VSP_BEM_OPTIONS_SCREEN
r""" Blade element method options screen"""
VSP_CFD_MESH_SCREEN = _vsp.VSP_CFD_MESH_SCREEN
r""" CFD Mesh screen"""
VSP_CLIPPING_SCREEN = _vsp.VSP_CLIPPING_SCREEN
r""" Clipping screen"""
VSP_COMP_GEOM_SCREEN = _vsp.VSP_COMP_GEOM_SCREEN
r""" CompGeom screen"""
VSP_COR_SCREEN = _vsp.VSP_COR_SCREEN
r""" Center of rotation screen"""
VSP_CURVE_EDIT_SCREEN = _vsp.VSP_CURVE_EDIT_SCREEN
r""" Curve edit screen"""
VSP_DEGEN_GEOM_SCREEN = _vsp.VSP_DEGEN_GEOM_SCREEN
r""" Degen geom screen"""
VSP_DESIGN_VAR_SCREEN = _vsp.VSP_DESIGN_VAR_SCREEN
r""" Design variables screen"""
VSP_DXF_OPTIONS_SCREEN = _vsp.VSP_DXF_OPTIONS_SCREEN
r""" DXF options screen"""
VSP_EXPORT_SCREEN = _vsp.VSP_EXPORT_SCREEN
r""" Export screen"""
VSP_FEA_PART_EDIT_SCREEN = _vsp.VSP_FEA_PART_EDIT_SCREEN
r""" FEA Part edit screen"""
VSP_FEA_XSEC_SCREEN = _vsp.VSP_FEA_XSEC_SCREEN
r""" FEA XSec screen"""
VSP_FIT_MODEL_SCREEN = _vsp.VSP_FIT_MODEL_SCREEN
r""" Fit model screen"""
VSP_IGES_OPTIONS_SCREEN = _vsp.VSP_IGES_OPTIONS_SCREEN
r""" IGES options screen"""
VSP_IGES_STRUCTURE_OPTIONS_SCREEN = _vsp.VSP_IGES_STRUCTURE_OPTIONS_SCREEN
r""" IGES structure options screen"""
VSP_EXPORT_CUSTOM_SCRIPT = _vsp.VSP_EXPORT_CUSTOM_SCRIPT
r""" Custom geom export screen"""
VSP_IMPORT_SCREEN = _vsp.VSP_IMPORT_SCREEN
r""" Import screen"""
VSP_LIGHTING_SCREEN = _vsp.VSP_LIGHTING_SCREEN
r""" Lighting screen"""
VSP_MANAGE_GEOM_SCREEN = _vsp.VSP_MANAGE_GEOM_SCREEN
r""" Manage geom screen"""
VSP_MANAGE_TEXTURE_SCREEN = _vsp.VSP_MANAGE_TEXTURE_SCREEN
r""" Texture mapping screen"""
VSP_MASS_PROP_SCREEN = _vsp.VSP_MASS_PROP_SCREEN
r""" Mass properties screen"""
VSP_MATERIAL_EDIT_SCREEN = _vsp.VSP_MATERIAL_EDIT_SCREEN
r""" Material edit screen"""
VSP_MEASURE_SCREEN = _vsp.VSP_MEASURE_SCREEN
r""" Measure screen"""
VSP_NERF_MANAGE_GEOM_SCREEN = _vsp.VSP_NERF_MANAGE_GEOM_SCREEN
r""" NERF'ed (limited to make safe) Manage geom screen"""
VSP_SNAP_TO_SCREEN = _vsp.VSP_SNAP_TO_SCREEN
r""" Snap to screen"""
VSP_PARASITE_DRAG_SCREEN = _vsp.VSP_PARASITE_DRAG_SCREEN
r""" Parasite drg screen"""
VSP_PARM_DEBUG_SCREEN = _vsp.VSP_PARM_DEBUG_SCREEN
r""" Parameter debug screen"""
VSP_PARM_LINK_SCREEN = _vsp.VSP_PARM_LINK_SCREEN
r""" Parameter linking screen"""
VSP_PARM_SCREEN = _vsp.VSP_PARM_SCREEN
r""" Parameter screen"""
VSP_PICK_SET_SCREEN = _vsp.VSP_PICK_SET_SCREEN
r""" Pick set screen"""
VSP_PREFERENCES_SCREEN = _vsp.VSP_PREFERENCES_SCREEN
r""" Preferences screen"""
VSP_PROJECTION_SCREEN = _vsp.VSP_PROJECTION_SCREEN
r""" Projected area screen"""
VSP_PSLICE_SCREEN = _vsp.VSP_PSLICE_SCREEN
r""" Planar slicing screen"""
VSP_SCREENSHOT_SCREEN = _vsp.VSP_SCREENSHOT_SCREEN
r""" Screenshot screen"""
VSP_SELECT_FILE_SCREEN = _vsp.VSP_SELECT_FILE_SCREEN
r""" Select file screen"""
VSP_SET_EDITOR_SCREEN = _vsp.VSP_SET_EDITOR_SCREEN
r""" Set editor screen"""
VSP_STEP_OPTIONS_SCREEN = _vsp.VSP_STEP_OPTIONS_SCREEN
r""" STEP options screen"""
VSP_STEP_STRUCTURE_OPTIONS_SCREEN = _vsp.VSP_STEP_STRUCTURE_OPTIONS_SCREEN
r""" STEP structure options screen"""
VSP_STL_OPTIONS_SCREEN = _vsp.VSP_STL_OPTIONS_SCREEN
r""" STL options screen"""
VSP_STRUCT_SCREEN = _vsp.VSP_STRUCT_SCREEN
r""" Structure definition screen"""
VSP_STRUCT_ASSEMBLY_SCREEN = _vsp.VSP_STRUCT_ASSEMBLY_SCREEN
r""" Structure assembly screen"""
VSP_SURFACE_INTERSECTION_SCREEN = _vsp.VSP_SURFACE_INTERSECTION_SCREEN
r""" Surface intersection screen"""
VSP_SVG_OPTIONS_SCREEN = _vsp.VSP_SVG_OPTIONS_SCREEN
r""" SVG options screen"""
VSP_USER_PARM_SCREEN = _vsp.VSP_USER_PARM_SCREEN
r""" User parameter screen"""
VSP_VAR_PRESET_SCREEN = _vsp.VSP_VAR_PRESET_SCREEN
r""" Variable presets screen"""
VSP_VIEW_SCREEN = _vsp.VSP_VIEW_SCREEN
r""" Adjust viewpoint screen"""
VSP_VSPAERO_PLOT_SCREEN = _vsp.VSP_VSPAERO_PLOT_SCREEN
r""" VSPAERO results manager screen"""
VSP_VSPAERO_SCREEN = _vsp.VSP_VSPAERO_SCREEN
r""" VSPAERO screen"""
VSP_XSEC_SCREEN = _vsp.VSP_XSEC_SCREEN
r""" XSec screen"""
VSP_WAVEDRAG_SCREEN = _vsp.VSP_WAVEDRAG_SCREEN
r""" Wave drag screen"""
VSP_MAIN_SCREEN = _vsp.VSP_MAIN_SCREEN
r""" Main screen"""
VSP_NUM_SCREENS = _vsp.VSP_NUM_SCREENS
r""" Number of screens"""
VSP_ALL_SCREENS = _vsp.VSP_ALL_SCREENS
r""" Flag for all screens"""
EDIT_XSEC_CIRCLE = _vsp.EDIT_XSEC_CIRCLE
r""" Circle initialized as cubic Bezier type"""
EDIT_XSEC_ELLIPSE = _vsp.EDIT_XSEC_ELLIPSE
r""" Ellipse initialized as PCHIP type"""
EDIT_XSEC_RECTANGLE = _vsp.EDIT_XSEC_RECTANGLE
r""" Rectangle initialized as linear type"""
IMPORT_STL = _vsp.IMPORT_STL
r""" Stereolith (*.stl) import"""
IMPORT_NASCART = _vsp.IMPORT_NASCART
r""" NASCART (*.dat) import"""
IMPORT_CART3D_TRI = _vsp.IMPORT_CART3D_TRI
r""" Cart3D (*.try) import"""
IMPORT_XSEC_MESH = _vsp.IMPORT_XSEC_MESH
r""" XSec as Tri Mesh (*.hrm) import"""
IMPORT_PTS = _vsp.IMPORT_PTS
r""" Point Cloud (*.pts) import"""
IMPORT_V2 = _vsp.IMPORT_V2
r""" OpenVSP v2 (*.vsp) import"""
IMPORT_BEM = _vsp.IMPORT_BEM
r""" Blade Element (*.bem) import"""
IMPORT_XSEC_WIRE = _vsp.IMPORT_XSEC_WIRE
r""" XSec as Wireframe (*.hrm) import"""
IMPORT_P3D_WIRE = _vsp.IMPORT_P3D_WIRE
r""" Plot3D as Wireframe (*.p3d) import"""
INTERSECT_SRF_FILE_NAME = _vsp.INTERSECT_SRF_FILE_NAME
r""" SRF intersection file type"""
INTERSECT_CURV_FILE_NAME = _vsp.INTERSECT_CURV_FILE_NAME
r""" CURV intersection file type"""
INTERSECT_PLOT3D_FILE_NAME = _vsp.INTERSECT_PLOT3D_FILE_NAME
r""" PLOT3D intersection file type"""
INTERSECT_IGES_FILE_NAME = _vsp.INTERSECT_IGES_FILE_NAME
r""" IGES intersection file type"""
INTERSECT_STEP_FILE_NAME = _vsp.INTERSECT_STEP_FILE_NAME
r""" STEP intersection file type"""
INTERSECT_NUM_FILE_NAMES = _vsp.INTERSECT_NUM_FILE_NAMES
r""" Number of surface intersection file types"""
LEN_MM = _vsp.LEN_MM
r""" Millimeter"""
LEN_CM = _vsp.LEN_CM
r""" Centimeter"""
LEN_M = _vsp.LEN_M
r""" Meter"""
LEN_IN = _vsp.LEN_IN
r""" Inch"""
LEN_FT = _vsp.LEN_FT
r""" Feet"""
LEN_YD = _vsp.LEN_YD
r""" Yard"""
LEN_UNITLESS = _vsp.LEN_UNITLESS
r""" Unitless"""
NUM_LEN_UNIT = _vsp.NUM_LEN_UNIT
r""" Number of length unit types"""
MASS_UNIT_G = _vsp.MASS_UNIT_G
r""" Gram"""
MASS_UNIT_KG = _vsp.MASS_UNIT_KG
r""" Kilogram"""
MASS_UNIT_TONNE = _vsp.MASS_UNIT_TONNE
r""" Tonne"""
MASS_UNIT_LBM = _vsp.MASS_UNIT_LBM
r""" Pound-mass"""
MASS_UNIT_SLUG = _vsp.MASS_UNIT_SLUG
r""" Slug"""
MASS_LBFSEC2IN = _vsp.MASS_LBFSEC2IN
r""" lbf*sec^2/in"""
NUM_MASS_UNIT = _vsp.NUM_MASS_UNIT
r""" Number of mass unit types"""
NO_REASON = _vsp.NO_REASON
r""" No reason determined."""
MAX_LEN_CONSTRAINT = _vsp.MAX_LEN_CONSTRAINT
r""" Maximum edge length."""
CURV_GAP = _vsp.CURV_GAP
r""" Maximum gap curvature based criteria."""
CURV_NCIRCSEG = _vsp.CURV_NCIRCSEG
r""" Minimum number of segments to define a circle curvature based criteria."""
SOURCES = _vsp.SOURCES
r""" Mesh sources."""
MIN_LEN_CONSTRAINT = _vsp.MIN_LEN_CONSTRAINT
r""" Minimum edge length."""
MIN_LEN_CONSTRAINT_CURV_GAP = _vsp.MIN_LEN_CONSTRAINT_CURV_GAP
r""" Maximum gap constrained by minimum length."""
MIN_LEN_CONSTRAINT_CURV_NCIRCSEG = _vsp.MIN_LEN_CONSTRAINT_CURV_NCIRCSEG
r""" Number of segments to define a circle constrained by minimum length."""
MIN_LEN_CONSTRAINT_SOURCES = _vsp.MIN_LEN_CONSTRAINT_SOURCES
r""" Mesh sources constrained by minimum length (not applied)."""
GROW_LIMIT_MAX_LEN_CONSTRAINT = _vsp.GROW_LIMIT_MAX_LEN_CONSTRAINT
r""" Maximum growth limit from maximum edge length (not used, growth limited small to large)."""
GROW_LIMIT_CURV_GAP = _vsp.GROW_LIMIT_CURV_GAP
r""" Maximum growth limit from maximum gap."""
GROW_LIMIT_CURV_NCIRCSEG = _vsp.GROW_LIMIT_CURV_NCIRCSEG
r""" Maximum growth limit from number of segments to define a circle."""
GROW_LIMIT_SOURCES = _vsp.GROW_LIMIT_SOURCES
r""" Maximum growth limit from mesh sources."""
GROW_LIMIT_MIN_LEN_CONSTRAINT = _vsp.GROW_LIMIT_MIN_LEN_CONSTRAINT
r""" Maximum growth limit from minimum length constraint."""
GROW_LIMIT_MIN_LEN_CONSTRAINT_CURV_GAP = _vsp.GROW_LIMIT_MIN_LEN_CONSTRAINT_CURV_GAP
r""" Maximum growth limit from maximum gap constrained by minimum length."""
GROW_LIMIT_MIN_LEN_CONSTRAINT_CURV_NCIRCSEG = _vsp.GROW_LIMIT_MIN_LEN_CONSTRAINT_CURV_NCIRCSEG
r""" Maximum growth limit from number of segments to define a circle constrained by minimum length."""
GROW_LIMIT_MIN_LEN_CONSTRAINT_SOURCES = _vsp.GROW_LIMIT_MIN_LEN_CONSTRAINT_SOURCES
r""" Maximum growth limit from sources constrained by minimum length."""
NUM_MESH_REASON = _vsp.NUM_MESH_REASON
r""" Number of reasons that can set the mesh local minimum edge length."""
MIN_LEN_INCREMENT = _vsp.MIN_LEN_INCREMENT
r""" Reason increment when adding minimum length constraint."""
GROW_LIMIT_INCREMENT = _vsp.GROW_LIMIT_INCREMENT
r""" Reason increment when adding growth limit constraint."""
MIN_GROW_LIMIT = _vsp.MIN_GROW_LIMIT
r""" Reason marker for minimum reason to apply growth limit."""
PARM_DOUBLE_TYPE = _vsp.PARM_DOUBLE_TYPE
r""" Double Parm type (Parm)"""
PARM_INT_TYPE = _vsp.PARM_INT_TYPE
r""" Integer Parm type (IntParm)"""
PARM_BOOL_TYPE = _vsp.PARM_BOOL_TYPE
r""" Bool Parm type (BoolParm)"""
PARM_FRACTION_TYPE = _vsp.PARM_FRACTION_TYPE
r""" Fraction Parm type (FractionParm)"""
PARM_LIMITED_INT_TYPE = _vsp.PARM_LIMITED_INT_TYPE
r""" Limited integer Parm type (LimIntParm)"""
PARM_NOTEQ_TYPE = _vsp.PARM_NOTEQ_TYPE
r""" Not equal Parm type (NotEqParm)"""
PARM_POWER_INT_TYPE = _vsp.PARM_POWER_INT_TYPE
r""" Power integer Parm type (PowIntParm)"""
PATCH_NONE = _vsp.PATCH_NONE
r""" No patch"""
PATCH_POINT = _vsp.PATCH_POINT
r""" Point patch type"""
PATCH_LINE = _vsp.PATCH_LINE
r""" Line patch type"""
PATCH_COPY = _vsp.PATCH_COPY
r""" Copy patch type"""
PATCH_HALFWAY = _vsp.PATCH_HALFWAY
r""" Halfway patch type"""
PATCH_NUM_TYPES = _vsp.PATCH_NUM_TYPES
r""" Number of patch types"""
LINEAR = _vsp.LINEAR
r""" Linear curve type"""
PCHIP = _vsp.PCHIP
r""" Piecewise Cubic Hermite Interpolating Polynomial curve type"""
CEDIT = _vsp.CEDIT
r""" Cubic Bezier curve type"""
APPROX_CEDIT = _vsp.APPROX_CEDIT
r""" Approximate curve as Cubic Bezier"""
NUM_PCURV_TYPE = _vsp.NUM_PCURV_TYPE
r""" Number of curve types"""
PRES_UNIT_PSF = _vsp.PRES_UNIT_PSF
r""" Pounds per square foot"""
PRES_UNIT_PSI = _vsp.PRES_UNIT_PSI
r""" Pounds per square inch"""
PRES_UNIT_BA = _vsp.PRES_UNIT_BA
r""" Barye"""
PRES_UNIT_PA = _vsp.PRES_UNIT_PA
r""" Pascal"""
PRES_UNIT_KPA = _vsp.PRES_UNIT_KPA
r""" Kilopascal"""
PRES_UNIT_MPA = _vsp.PRES_UNIT_MPA
r""" Megapascal"""
PRES_UNIT_INCHHG = _vsp.PRES_UNIT_INCHHG
r""" Inch of mercury"""
PRES_UNIT_MMHG = _vsp.PRES_UNIT_MMHG
r""" Millimeter of mercury"""
PRES_UNIT_MMH20 = _vsp.PRES_UNIT_MMH20
r""" Millimeter of water"""
PRES_UNIT_MB = _vsp.PRES_UNIT_MB
r""" Millibar"""
PRES_UNIT_ATM = _vsp.PRES_UNIT_ATM
r""" Atmosphere"""
NUM_PRES_UNIT = _vsp.NUM_PRES_UNIT
r""" Number of pressure unit choices"""
NO_BOUNDARY = _vsp.NO_BOUNDARY
r""" No boundary"""
SET_BOUNDARY = _vsp.SET_BOUNDARY
r""" Set boundary"""
GEOM_BOUNDARY = _vsp.GEOM_BOUNDARY
r""" Geom boundary"""
NUM_PROJ_BNDY_OPTIONS = _vsp.NUM_PROJ_BNDY_OPTIONS
r""" Number of projected area boundary options"""
X_PROJ = _vsp.X_PROJ
r""" Project in X axis direction"""
Y_PROJ = _vsp.Y_PROJ
r""" Project in Y axis direction"""
Z_PROJ = _vsp.Z_PROJ
r""" Project in Z axis direction"""
GEOM_PROJ = _vsp.GEOM_PROJ
r""" Project toward a Geom"""
VEC_PROJ = _vsp.VEC_PROJ
r""" Project along a 3D vector"""
NUM_PROJ_DIR_OPTIONS = _vsp.NUM_PROJ_DIR_OPTIONS
r""" Number of Projected Area direction types"""
SET_TARGET = _vsp.SET_TARGET
r""" Set target type"""
GEOM_TARGET = _vsp.GEOM_TARGET
r""" Geom target type"""
NUM_PROJ_TGT_OPTIONS = _vsp.NUM_PROJ_TGT_OPTIONS
r""" Number of Projected Area target types"""
PROP_BLADES = _vsp.PROP_BLADES
r""" Propeller Geom is defined by individual propeller blades"""
PROP_BOTH = _vsp.PROP_BOTH
r""" Propeller Geom is defined by blades and a disk together"""
PROP_DISK = _vsp.PROP_DISK
r""" Propeller Geom is defined by a flat circular disk"""
PROP_CHORD = _vsp.PROP_CHORD
r""" Chord parameterization"""
PROP_TWIST = _vsp.PROP_TWIST
r""" Twist parameterization"""
PROP_RAKE = _vsp.PROP_RAKE
r""" Rake parameterization"""
PROP_SKEW = _vsp.PROP_SKEW
r""" Skew parameterization"""
PROP_SWEEP = _vsp.PROP_SWEEP
r""" Sweep parameterization"""
PROP_THICK = _vsp.PROP_THICK
r""" Thickness parameterization"""
PROP_CLI = _vsp.PROP_CLI
r""" Induced lift coefficient parameterization"""
PROP_AXIAL = _vsp.PROP_AXIAL
r""" Axial parameterization"""
PROP_TANGENTIAL = _vsp.PROP_TANGENTIAL
r""" Tangential parameterization"""
NUM_PROP_PCURVE = _vsp.NUM_PROP_PCURVE
r""" Number of propeller blade curve parameterization options"""
REORDER_MOVE_UP = _vsp.REORDER_MOVE_UP
r""" Move up one position"""
REORDER_MOVE_DOWN = _vsp.REORDER_MOVE_DOWN
r""" Move down one position"""
REORDER_MOVE_TOP = _vsp.REORDER_MOVE_TOP
r""" Move to top"""
REORDER_MOVE_BOTTOM = _vsp.REORDER_MOVE_BOTTOM
r""" Move to bottom"""
NUM_REORDER_TYPES = _vsp.NUM_REORDER_TYPES
r""" Number reordering instructions"""
MANUAL_REF = _vsp.MANUAL_REF
r""" Manually specify the reference areas and lengths"""
COMPONENT_REF = _vsp.COMPONENT_REF
r""" Use a particular wing to calculate the reference area and lengths"""
NUM_REF_TYPES = _vsp.NUM_REF_TYPES
r""" Number of wing reference types"""
INVALID_TYPE = _vsp.INVALID_TYPE
r""" Invalid result data type"""
INT_DATA = _vsp.INT_DATA
r""" Integer result data type"""
DOUBLE_DATA = _vsp.DOUBLE_DATA
r""" Double result data type"""
STRING_DATA = _vsp.STRING_DATA
r""" String result data type"""
VEC3D_DATA = _vsp.VEC3D_DATA
r""" Vec3d result data type"""
DOUBLE_MATRIX_DATA = _vsp.DOUBLE_MATRIX_DATA
r""" Double matrix result data type"""
MESH_INDEXED_TRI = _vsp.MESH_INDEXED_TRI
r""" Indexed triangulated mesh Geom type"""
MESH_SLICE_TRI = _vsp.MESH_SLICE_TRI
r""" Sliced Triangulated mesh Geom type"""
GEOM_XSECS = _vsp.GEOM_XSECS
r""" GeomXSec Geom type"""
MESH_INDEX_AND_SLICE_TRI = _vsp.MESH_INDEX_AND_SLICE_TRI
r""" Both indexed and sliced triangulated mesh Geom type"""
RHO_UNIT_SLUG_FT3 = _vsp.RHO_UNIT_SLUG_FT3
r""" Slug per cubic foot"""
RHO_UNIT_G_CM3 = _vsp.RHO_UNIT_G_CM3
r""" Gram per cubic centimeter"""
RHO_UNIT_KG_M3 = _vsp.RHO_UNIT_KG_M3
r""" Kilogram per cubic meter"""
RHO_UNIT_TONNE_MM3 = _vsp.RHO_UNIT_TONNE_MM3
r""" Tonne per cubic millimeter"""
RHO_UNIT_LBM_FT3 = _vsp.RHO_UNIT_LBM_FT3
r""" Pound-mass per cubic foot"""
RHO_UNIT_LBFSEC2_IN4 = _vsp.RHO_UNIT_LBFSEC2_IN4
r""" Pound-force-second squared per inch to the fourth"""
RHO_UNIT_LBM_IN3 = _vsp.RHO_UNIT_LBM_IN3
r""" Pound-mass per cubic inch"""
NUM_RHO_UNIT = _vsp.NUM_RHO_UNIT
r""" Number of density unit options"""
SCALE_WIDTH = _vsp.SCALE_WIDTH
r""" Scale image to match desired width"""
SCALE_HEIGHT = _vsp.SCALE_HEIGHT
r""" Scale image to match desired height"""
SCALE_WIDTH_HEIGHT = _vsp.SCALE_WIDTH_HEIGHT
r""" Scale image to match desired width and height"""
SCALE_RESOLUTION = _vsp.SCALE_RESOLUTION
r""" Scale image to specified resolution"""
NUM_SCALE_TYPES = _vsp.NUM_SCALE_TYPES
r""" Number of ways to scale 3D background image."""
SET_NONE = _vsp.SET_NONE
r""" None set"""
SET_ALL = _vsp.SET_ALL
r""" All set"""
SET_SHOWN = _vsp.SET_SHOWN
r""" Shown set"""
SET_NOT_SHOWN = _vsp.SET_NOT_SHOWN
r""" Not shown set"""
SET_FIRST_USER = _vsp.SET_FIRST_USER
r""" First user-defined set"""
MIN_NUM_USER = _vsp.MIN_NUM_USER
r""" Minimum number of user sets"""
MAX_NUM_SETS = _vsp.MAX_NUM_SETS
r""" Maximum possible number of sets"""
STEP_SHELL = _vsp.STEP_SHELL
r""" Manifold shell surface STEP file representation"""
STEP_BREP = _vsp.STEP_BREP
r""" Manifold solid BREP STEP file representation"""
SS_INC_TREAT_AS_PARENT = _vsp.SS_INC_TREAT_AS_PARENT
r""" Treat the sub-surface the same as the parent"""
SS_INC_SEPARATE_TREATMENT = _vsp.SS_INC_SEPARATE_TREATMENT
r""" Treat the sub-surface separately from the parent"""
SS_INC_ZERO_DRAG = _vsp.SS_INC_ZERO_DRAG
r""" No drag contribution for the sub-surface"""
INSIDE = _vsp.INSIDE
r""" The interior of the sub-surface is its surface"""
OUTSIDE = _vsp.OUTSIDE
r""" The exterior of the sub-surface is its surface"""
NONE = _vsp.NONE
r""" No part of the parent surface belongs to the sub-surface"""
CONST_U = _vsp.CONST_U
r""" Constant U sub-surface"""
CONST_W = _vsp.CONST_W
r""" Constant W sub-surface"""
SS_LINE = _vsp.SS_LINE
r""" Line sub-surface type"""
SS_RECTANGLE = _vsp.SS_RECTANGLE
r""" Rectangle sub-surface type"""
SS_ELLIPSE = _vsp.SS_ELLIPSE
r""" Ellipse sub-surface type"""
SS_CONTROL = _vsp.SS_CONTROL
r""" Control sub-surface type"""
SS_LINE_ARRAY = _vsp.SS_LINE_ARRAY
r""" Line array sub-surface type"""
SS_FINITE_LINE = _vsp.SS_FINITE_LINE
r""" Finite line sub-surface type"""
SS_NUM_TYPES = _vsp.SS_NUM_TYPES
r""" Number of sub-surface types"""
SYM_XY = _vsp.SYM_XY
r""" XY planar symmetry."""
SYM_XZ = _vsp.SYM_XZ
r""" XZ planar symmetry."""
SYM_YZ = _vsp.SYM_YZ
r""" YZ planar symmetry."""
SYM_ROT_X = _vsp.SYM_ROT_X
r""" X rotational symmetry."""
SYM_ROT_Y = _vsp.SYM_ROT_Y
r""" Y rotational symmetry."""
SYM_ROT_Z = _vsp.SYM_ROT_Z
r""" Z rotational symmetry."""
SYM_PLANAR_TYPES = _vsp.SYM_PLANAR_TYPES
r""" Number of planar symmetry types."""
SYM_NUM_TYPES = _vsp.SYM_NUM_TYPES
r""" Number of symmetry types."""
SYM_NONE = _vsp.SYM_NONE
r""" No cross section symmetry."""
SYM_RL = _vsp.SYM_RL
r""" Right/left cross section symmetry."""
SYM_TB = _vsp.SYM_TB
r""" Top/bottom cross section symmetry."""
SYM_ALL = _vsp.SYM_ALL
r""" All cross section symmetry."""
TEMP_UNIT_K = _vsp.TEMP_UNIT_K
r""" Kelvin"""
TEMP_UNIT_C = _vsp.TEMP_UNIT_C
r""" Celsius"""
TEMP_UNIT_F = _vsp.TEMP_UNIT_F
r""" Fahrenheit"""
TEMP_UNIT_R = _vsp.TEMP_UNIT_R
r""" Rankine"""
NUM_TEMP_UNIT = _vsp.NUM_TEMP_UNIT
r""" Number of temperature unit choices"""
V_UNIT_FT_S = _vsp.V_UNIT_FT_S
r""" Feet per second"""
V_UNIT_M_S = _vsp.V_UNIT_M_S
r""" Meter per second"""
V_UNIT_MPH = _vsp.V_UNIT_MPH
r""" Mile per hour"""
V_UNIT_KM_HR = _vsp.V_UNIT_KM_HR
r""" Kilometer per hour"""
V_UNIT_KEAS = _vsp.V_UNIT_KEAS
r""" Knots equivalent airspeed"""
V_UNIT_KTAS = _vsp.V_UNIT_KTAS
r""" Knots true airspeed"""
V_UNIT_MACH = _vsp.V_UNIT_MACH
r""" Mach"""
VIEW_1 = _vsp.VIEW_1
r""" One 2D view"""
VIEW_2HOR = _vsp.VIEW_2HOR
r""" Two horizontal 2D views"""
VIEW_2VER = _vsp.VIEW_2VER
r""" Two vertical 2D views"""
VIEW_4 = _vsp.VIEW_4
r""" Four 2D views"""
ROT_0 = _vsp.ROT_0
r""" No rotation"""
ROT_90 = _vsp.ROT_90
r""" 90 degree rotation"""
ROT_180 = _vsp.ROT_180
r""" 180 degree rotation"""
ROT_270 = _vsp.ROT_270
r""" 270 degree rotation"""
VIEW_LEFT = _vsp.VIEW_LEFT
r""" Left 2D view type"""
VIEW_RIGHT = _vsp.VIEW_RIGHT
r""" Right 2D view type"""
VIEW_TOP = _vsp.VIEW_TOP
r""" Top 2D view type"""
VIEW_BOTTOM = _vsp.VIEW_BOTTOM
r""" Bottom 2D view type"""
VIEW_FRONT = _vsp.VIEW_FRONT
r""" Front 2D view type"""
VIEW_REAR = _vsp.VIEW_REAR
r""" Rear 2D view type"""
VIEW_NONE = _vsp.VIEW_NONE
r""" No 2D view type"""
VIEW_NUM_TYPES = _vsp.VIEW_NUM_TYPES
r""" Number of 2D view types"""
VORTEX_LATTICE = _vsp.VORTEX_LATTICE
r""" VSPAERO vortex lattice method"""
PANEL = _vsp.PANEL
r""" VSPAERO panel method"""
NOISE_FLYBY = _vsp.NOISE_FLYBY
r""" Set up fly by noise analysis in VSPAERO for PSU-WOPWOP"""
NOISE_FOOTPRINT = _vsp.NOISE_FOOTPRINT
r""" Set up footprint noise analysis in VSPAERO for PSU-WOPWOP"""
NOISE_STEADY = _vsp.NOISE_STEADY
r""" Set up steady state noise analysis in VSPAERO for PSU-WOPWOP"""
NOISE_SI = _vsp.NOISE_SI
r""" Assume geometry and VSPAERO inputs in SI (m N kg s) for PSU-WOPWOP"""
NOISE_ENGLISH = _vsp.NOISE_ENGLISH
r""" Assume geometry and VSPAERO inputs in english (ft lbf slug s) units, will convert to SI (m N kg s) for PSU-WOPWOP"""
PRECON_MATRIX = _vsp.PRECON_MATRIX
r""" Matrix preconditioner"""
PRECON_JACOBI = _vsp.PRECON_JACOBI
r""" Jacobi preconditioner"""
PRECON_SSOR = _vsp.PRECON_SSOR
r""" Symmetric successive over-relaxation preconditioner"""
STABILITY_OFF = _vsp.STABILITY_OFF
r""" No stability analysis (off)"""
STABILITY_DEFAULT = _vsp.STABILITY_DEFAULT
r""" Steady 6DOF stability analysis"""
STABILITY_P_ANALYSIS = _vsp.STABILITY_P_ANALYSIS
r""" Unsteady roll stability analysis"""
STABILITY_Q_ANALYSIS = _vsp.STABILITY_Q_ANALYSIS
r""" Unsteady pitch stability analysis"""
STABILITY_R_ANALYSIS = _vsp.STABILITY_R_ANALYSIS
r""" Unsteady yaw stability analysis"""
STABILITY_PITCH = _vsp.STABILITY_PITCH
r""" Simplified pitch stability analysis"""
STABILITY_NUM_TYPES = _vsp.STABILITY_NUM_TYPES
r""" Number of stability analysis types"""
CLMAX_OFF = _vsp.CLMAX_OFF
r""" Stall modeling off (Cl Max = 0)"""
CLMAX_2D = _vsp.CLMAX_2D
r""" 2D Cl Max stall modeling with user defined value"""
CLMAX_CARLSON = _vsp.CLMAX_CARLSON
r""" Carlson's Pressure Correlation"""
CFD_NORMAL = _vsp.CFD_NORMAL
r""" Normal CFD Mesh surface"""
CFD_NEGATIVE = _vsp.CFD_NEGATIVE
r""" Negative volume CFD Mesh surface"""
CFD_TRANSPARENT = _vsp.CFD_TRANSPARENT
r""" Transparent CFD Mesh surface"""
CFD_STRUCTURE = _vsp.CFD_STRUCTURE
r""" FEA structure CFD Mesh surface"""
CFD_STIFFENER = _vsp.CFD_STIFFENER
r""" FEA stiffener CFD Mesh surface"""
CFD_MEASURE_DUCT = _vsp.CFD_MEASURE_DUCT
r""" Measure duct cross sectional area surface"""
CFD_NUM_TYPES = _vsp.CFD_NUM_TYPES
r""" Number of CFD Mesh surface types"""
NORMAL_SURF = _vsp.NORMAL_SURF
r""" Normal VSP surface"""
WING_SURF = _vsp.WING_SURF
r""" Wing VSP surface"""
DISK_SURF = _vsp.DISK_SURF
r""" Disk VSP surface"""
NUM_SURF_TYPES = _vsp.NUM_SURF_TYPES
r""" Number of VSP surface types"""
W_RIGHT_0 = _vsp.W_RIGHT_0
r""" Chevron start/ends at right (W = 0) of cross section"""
W_BOTTOM = _vsp.W_BOTTOM
r""" Chevron start/ends at bottom of cross section"""
W_LEFT = _vsp.W_LEFT
r""" Chevron start/ends at left of cross section"""
W_TOP = _vsp.W_TOP
r""" Chevron start/ends at top of cross section"""
W_RIGHT_1 = _vsp.W_RIGHT_1
r""" Chevron start/ends at right (W = 1) of cross section"""
W_FREE = _vsp.W_FREE
r""" Chevron start/ends at user specified point on cross section"""
BLEND_FREE = _vsp.BLEND_FREE
r""" Free blending"""
BLEND_ANGLES = _vsp.BLEND_ANGLES
r""" Blend based on angles (sweep & dihedral)"""
BLEND_MATCH_IN_LE_TRAP = _vsp.BLEND_MATCH_IN_LE_TRAP
r""" Match inboard leading edge trapezoid"""
BLEND_MATCH_IN_TE_TRAP = _vsp.BLEND_MATCH_IN_TE_TRAP
r""" Match inboard trailing edge trapezoid"""
BLEND_MATCH_OUT_LE_TRAP = _vsp.BLEND_MATCH_OUT_LE_TRAP
r""" Match outboard leading edge trapezoid"""
BLEND_MATCH_OUT_TE_TRAP = _vsp.BLEND_MATCH_OUT_TE_TRAP
r""" Match outboard trailing edge trapezoid"""
BLEND_MATCH_IN_ANGLES = _vsp.BLEND_MATCH_IN_ANGLES
r""" Match inboard angles"""
BLEND_MATCH_LE_ANGLES = _vsp.BLEND_MATCH_LE_ANGLES
r""" Match leading edge angles"""
BLEND_NUM_TYPES = _vsp.BLEND_NUM_TYPES
r""" Number of blending types"""
AR_WSECT_DRIVER = _vsp.AR_WSECT_DRIVER
r""" Aspect ratio driver"""
SPAN_WSECT_DRIVER = _vsp.SPAN_WSECT_DRIVER
r""" Span driver"""
AREA_WSECT_DRIVER = _vsp.AREA_WSECT_DRIVER
r""" Area driver"""
TAPER_WSECT_DRIVER = _vsp.TAPER_WSECT_DRIVER
r""" Taper driver"""
AVEC_WSECT_DRIVER = _vsp.AVEC_WSECT_DRIVER
r""" Average chord driver"""
ROOTC_WSECT_DRIVER = _vsp.ROOTC_WSECT_DRIVER
r""" Root chord driver"""
TIPC_WSECT_DRIVER = _vsp.TIPC_WSECT_DRIVER
r""" Tip chord driver"""
SECSWEEP_WSECT_DRIVER = _vsp.SECSWEEP_WSECT_DRIVER
r""" Section sweep driver"""
NUM_WSECT_DRIVER = _vsp.NUM_WSECT_DRIVER
r""" Number of wing section drivers"""
SWEEP_WSECT_DRIVER = _vsp.SWEEP_WSECT_DRIVER
SWEEPLOC_WSECT_DRIVER = _vsp.SWEEPLOC_WSECT_DRIVER
SECSWEEPLOC_WSECT_DRIVER = _vsp.SECSWEEPLOC_WSECT_DRIVER
XDDM_VAR = _vsp.XDDM_VAR
r""" Variable XDDM type"""
XDDM_CONST = _vsp.XDDM_CONST
r""" Constant XDDM type"""
CLOSE_NONE = _vsp.CLOSE_NONE
r""" No closure"""
CLOSE_SKEWLOW = _vsp.CLOSE_SKEWLOW
r""" Skew lower closure"""
CLOSE_SKEWUP = _vsp.CLOSE_SKEWUP
r""" Skew upper closure"""
CLOSE_SKEWBOTH = _vsp.CLOSE_SKEWBOTH
r""" Skew both closure"""
CLOSE_EXTRAP = _vsp.CLOSE_EXTRAP
r""" Extrapolate closure"""
CLOSE_NUM_TYPES = _vsp.CLOSE_NUM_TYPES
r""" Number of XSec closure types"""
XS_UNDEFINED = _vsp.XS_UNDEFINED
XS_POINT = _vsp.XS_POINT
r""" Point XSec"""
XS_CIRCLE = _vsp.XS_CIRCLE
r""" Circle XSec"""
XS_ELLIPSE = _vsp.XS_ELLIPSE
r""" Ellipse XSec"""
XS_SUPER_ELLIPSE = _vsp.XS_SUPER_ELLIPSE
r""" Super ellipse XSec"""
XS_ROUNDED_RECTANGLE = _vsp.XS_ROUNDED_RECTANGLE
r""" Rounded rectangle XSec"""
XS_GENERAL_FUSE = _vsp.XS_GENERAL_FUSE
r""" General fuselage XSec"""
XS_FILE_FUSE = _vsp.XS_FILE_FUSE
r""" Fuselage file XSec"""
XS_FOUR_SERIES = _vsp.XS_FOUR_SERIES
r""" Four series XSec"""
XS_SIX_SERIES = _vsp.XS_SIX_SERIES
r""" Six series XSec"""
XS_BICONVEX = _vsp.XS_BICONVEX
r""" Biconvex XSec"""
XS_WEDGE = _vsp.XS_WEDGE
r""" Wedge XSec"""
XS_EDIT_CURVE = _vsp.XS_EDIT_CURVE
r""" Generic Edit Curve XSec"""
XS_FILE_AIRFOIL = _vsp.XS_FILE_AIRFOIL
r""" Airfoil file XSec"""
XS_CST_AIRFOIL = _vsp.XS_CST_AIRFOIL
r""" CST airfoil XSec"""
XS_VKT_AIRFOIL = _vsp.XS_VKT_AIRFOIL
r""" VKT airfoil XSec"""
XS_FOUR_DIGIT_MOD = _vsp.XS_FOUR_DIGIT_MOD
r""" Four digit modified XSec"""
XS_FIVE_DIGIT = _vsp.XS_FIVE_DIGIT
r""" Five digit XSec"""
XS_FIVE_DIGIT_MOD = _vsp.XS_FIVE_DIGIT_MOD
r""" Five digit modified XSec"""
XS_ONE_SIX_SERIES = _vsp.XS_ONE_SIX_SERIES
r""" One six series XSec"""
XS_NUM_TYPES = _vsp.XS_NUM_TYPES
r""" Number of XSec types"""
WIDTH_XSEC_DRIVER = _vsp.WIDTH_XSEC_DRIVER
AREA_XSEC_DRIVER = _vsp.AREA_XSEC_DRIVER
HEIGHT_XSEC_DRIVER = _vsp.HEIGHT_XSEC_DRIVER
r""" Height driver"""
HWRATIO_XSEC_DRIVER = _vsp.HWRATIO_XSEC_DRIVER
r""" Height/width ratio driver"""
NUM_XSEC_DRIVER = _vsp.NUM_XSEC_DRIVER
r""" Number of XSec drivers"""
CIRCLE_NUM_XSEC_DRIVER = _vsp.CIRCLE_NUM_XSEC_DRIVER
XSEC_BOTH_SIDES = _vsp.XSEC_BOTH_SIDES
r""" Both sides"""
XSEC_LEFT_SIDE = _vsp.XSEC_LEFT_SIDE
r""" Left side"""
XSEC_RIGHT_SIDE = _vsp.XSEC_RIGHT_SIDE
r""" Right side"""
TRIM_NONE = _vsp.TRIM_NONE
r""" No trimming"""
TRIM_X = _vsp.TRIM_X
r""" Trim XSec by X"""
TRIM_THICK = _vsp.TRIM_THICK
r""" Trim XSec by thickness"""
TRIM_NUM_TYPES = _vsp.TRIM_NUM_TYPES
r""" Number of trimming types"""
XSEC_FUSE = _vsp.XSEC_FUSE
r""" Fuselage XSec Geom"""
XSEC_STACK = _vsp.XSEC_STACK
r""" Stack XSec Geom"""
XSEC_WING = _vsp.XSEC_WING
r""" Wing XSec Geom"""
XSEC_CUSTOM = _vsp.XSEC_CUSTOM
r""" Custom XSec Geom"""
XSEC_PROP = _vsp.XSEC_PROP
r""" Propeller XSec Geom"""
XSEC_NUM_TYPES = _vsp.XSEC_NUM_TYPES
r""" Number of XSec types"""
XS_SHIFT_LE = _vsp.XS_SHIFT_LE
r""" Shift leading edge"""
XS_SHIFT_MID = _vsp.XS_SHIFT_MID
XS_SHIFT_TE = _vsp.XS_SHIFT_TE

@client_wrap
def VSPCheckSetup():
    r"""
    Check if OpenVSP has been initialized successfully. If not, the OpenVSP instance will be exited. This call should be placed at the
    beginning of all API scripts.


    .. code-block:: python


        VSPCheckSetup()

        # Continue to do things...



    """
    return _vsp.VSPCheckSetup()

@client_wrap
def VSPRenew():
    r"""
    Clear and reinitialize OpenVSP to all default settings


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        SetParmVal( pod_id, "Y_Rel_Location", "XForm", 2.0 )

        VSPRenew()

        if  len(FindGeoms()) != 0 : print( "ERROR: VSPRenew" )


    """
    return _vsp.VSPRenew()

@client_wrap
def Update(update_managers=True):
    r"""
    Update the entire vehicle and all lower level children. An input, which is true by default, is available to specify
    if managers should be updated as well. The managers are typically updated by their respective GUI, so must be
    updated through the API as well to avoid unexpected behavior.


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        xsec_surf = GetXSecSurf( fid, 0 )           # Get First (and Only) XSec Surf

        num_xsecs = GetNumXSec( xsec_surf )

        #==== Set Tan Angles At Nose/Tail
        SetXSecTanAngles( GetXSec( xsec_surf, 0 ), XSEC_BOTH_SIDES, 90, -1.0e12, -1.0e12, -1.0e12 )
        SetXSecTanAngles( GetXSec( xsec_surf, num_xsecs - 1 ), XSEC_BOTH_SIDES, -90, -1.0e12, -1.0e12, -1.0e12 )

        Update()       # Force Surface Update


    :type update_managers: boolean, optional
    :param update_managers: Flag to indicate if managers should be updated
    """
    return _vsp.Update(update_managers)

@client_wrap
def VSPExit(error_code):
    r"""
    Exit the program with a specific error code
    :param [in]: error_code Error code
    """
    return _vsp.VSPExit(error_code)

@client_wrap
def GetAndResetUpdateCount():
    r"""
    Return the OpenVSP update count and also reset it to zero.

    The OpenVSP update count tracks how many times the GUI has been told to update screens (set to dirty).  It
    provides a simple means of testing whether the OpenVSP state has possibly changed (non-zero returned).

    :rtype: int
    :return: int OpenVSP update count
    """
    return _vsp.GetAndResetUpdateCount()

@client_wrap
def GetVSPVersion():
    r"""
    Get the version of the OpenVSP instance currently running


    .. code-block:: python

        print( "The current OpenVSP version is: ", False )

        print( GetVSPVersion() )


    :rtype: string
    :return: OpenVSP version string (i.e. "OpenVSP 3.17.1")
    """
    return _vsp.GetVSPVersion()

@client_wrap
def GetVSPVersionMajor():
    r"""
    Get the major version of the OpenVSP instance currently running as an integer


    .. code-block:: python

        print( "The current OpenVSP version is: ", False )

        major = GetVSPVersionMajor()
        minor = GetVSPVersionMinor()
        change = GetVSPVersionChange()

        print( f"{major}.{minor}.{change}" )


    :rtype: int
    :return: OpenVSP major version number (i.e. 3 in 3.X.Y)
    """
    return _vsp.GetVSPVersionMajor()

@client_wrap
def GetVSPVersionMinor():
    r"""
    Get the minor version of the OpenVSP instance currently running as an integer


    .. code-block:: python

        print( "The current OpenVSP version is: ", False )

        major = GetVSPVersionMajor()
        minor = GetVSPVersionMinor()
        change = GetVSPVersionChange()

        print( f"{major}.{minor}.{change}" )


    :rtype: int
    :return: OpenVSP minor version number (i.e. X in 3.X.Y)
    """
    return _vsp.GetVSPVersionMinor()

@client_wrap
def GetVSPVersionChange():
    r"""
    Get the change version of the OpenVSP instance currently running as an integer


    .. code-block:: python

        print( "The current OpenVSP version is: ", False )

        major = GetVSPVersionMajor()
        minor = GetVSPVersionMinor()
        change = GetVSPVersionChange()

        print( f"{major}.{minor}.{change}" )


    :rtype: int
    :return: OpenVSP change version number (i.e. Y in 3.X.Y)
    """
    return _vsp.GetVSPVersionChange()

@client_wrap
def GetVSPExePath():
    r"""
    Get the path to the OpenVSP executable. OpenVSP will assume that the VSPAERO, VSPSLICER, and VSPVIEWER are in the same directory unless
    instructed otherwise.


    .. code-block:: python

        print( "The current VSP executable path is: ", False )

        print( GetVSPExePath() )


    See also: SetVSPAEROPath, CheckForVSPAERO, GetVSPAEROPath
    :rtype: string
    :return: Path to the OpenVSP executable
    """
    return _vsp.GetVSPExePath()

@client_wrap
def SetVSPAEROPath(path):
    r"""
    Set the path to the VSPAERO executables (Solver, Viewer, and Slicer). By default, OpenVSP will assume that the VSPAERO executables are in the
    same directory as the VSP executable. However, this may need to be changed when using certain API languages like MATLAB and Python. For example,
    Python may treat the location of the Python executable as the VSP executable path, so either the VSPAERO executable needs to be moved to the same
    directory or this function can be called to tell Python where to look for VSPAERO.


    .. code-block:: python

        if  not CheckForVSPAERO( GetVSPExePath() ) :
            vspaero_path = "C:/Users/example_user/Documents/OpenVSP_3.4.5"
            SetVSPAEROPath( vspaero_path )


    See also: GetVSPExePath, CheckForVSPAERO, GetVSPAEROPath
    :param [in]: path Absolute path to directory containing VSPAERO executable
    :rtype: boolean
    :return: Flag that indicates whether or not the path was set correctly
    """
    return _vsp.SetVSPAEROPath(path)

@client_wrap
def GetVSPAEROPath():
    r"""
    Get the path that OpenVSP will use to look for all VSPAERO executables (Solver, Slicer, and Viewer) when attempting to execute
    VSPAERO. If the VSPAERO executables are not in this location, they must either be copied there or the VSPAERO path must be set
    using SetVSPAEROPath.


    .. code-block:: python

        if  not CheckForVSPAERO( GetVSPAEROPath() ) :
            print( "VSPAERO is not where OpenVSP thinks it is. I should move the VSPAERO executable or call SetVSPAEROPath." )


    See also: GetVSPExePath, CheckForVSPAERO, SetVSPAEROPath
    :rtype: string
    :return: Path OpenVSP will look for VSPAERO
    """
    return _vsp.GetVSPAEROPath()

@client_wrap
def CheckForVSPAERO(path):
    r"""
    Check if all VSPAERO executables (Solver, Viewer, and Slicer) are in a given directory. Note that this function will return false
    if only one or two VSPAERO executables are found. An error message will indicate the executables that are missing. This may be
    acceptable, as only the Solver is needed in all cases. The Viewer and Slicer may not be needed.


    .. code-block:: python

        vspaero_path = "C:/Users/example_user/Documents/OpenVSP_3.4.5"

        if  CheckForVSPAERO( vspaero_path ) :
            SetVSPAEROPath( vspaero_path )


    See also: GetVSPExePath, GetVSPAEROPath, SetVSPAEROPath
    :param [in]: path Absolute path to check for VSPAERO executables
    :rtype: boolean
    :return: Flag that indicates if all VSPAERO executables are found or not
    """
    return _vsp.CheckForVSPAERO(path)

@client_wrap
def RegisterCFDMeshAnalyses():
    r"""RegisterCFDMeshAnalyses()"""
    return _vsp.RegisterCFDMeshAnalyses()

@client_wrap
def ReadVSPFile(file_name):
    r"""
    Load an OpenVSP project from a VSP3 file


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        fname = "example_fuse.vsp3"

        SetVSP3FileName( fname )

        Update()

        #==== Save Vehicle to File ====//
        print( "\tSaving vehicle file to: ", False )

        print( fname )

        WriteVSPFile( GetVSPFileName(), SET_ALL )

        #==== Reset Geometry ====//
        print( "--->Resetting VSP model to blank slate\n" )

        ClearVSPModel()

        ReadVSPFile( fname )


    :param [in]: file_name *.vsp3 file name
    """
    return _vsp.ReadVSPFile(file_name)

@client_wrap
def WriteVSPFile(*args):
    r"""
    Save the current OpenVSP project to a VSP3 file


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        fname = "example_fuse.vsp3"

        SetVSP3FileName( fname )

        Update()

        #==== Save Vehicle to File ====//
        print( "\tSaving vehicle file to: ", False )

        print( fname )

        WriteVSPFile( GetVSPFileName(), SET_ALL )

        #==== Reset Geometry ====//
        print( "--->Resetting VSP model to blank slate\n" )

        ClearVSPModel()

        ReadVSPFile( fname )


    :param [in]: file_name *.vsp3 file name
    :param [in]: set Set index to write (i.e. SET_ALL)
    """
    return _vsp.WriteVSPFile(*args)

@client_wrap
def SetVSP3FileName(file_name):
    r"""
    Set the file name of a OpenVSP project


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        fname = "example_fuse.vsp3"

        SetVSP3FileName( fname )

        Update()

        #==== Save Vehicle to File ====//
        print( "\tSaving vehicle file to: ", False )

        print( fname )

        WriteVSPFile( GetVSPFileName(), SET_ALL )

        #==== Reset Geometry ====//
        print( "--->Resetting VSP model to blank slate\n" )

        ClearVSPModel()

        ReadVSPFile( fname )


    :param [in]: file_name File name
    """
    return _vsp.SetVSP3FileName(file_name)

@client_wrap
def GetVSPFileName():
    r"""
    Get the file name of the current OpenVSP project


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        fname = "example_fuse.vsp3"

        SetVSP3FileName( fname )

        Update()

        #==== Save Vehicle to File ====//
        print( "\tSaving vehicle file to: ", False )

        print( fname )

        WriteVSPFile( GetVSPFileName(), SET_ALL )


    :rtype: string
    :return: File name for the current OpenVSP project
    """
    return _vsp.GetVSPFileName()

@client_wrap
def ClearVSPModel():
    r"""
    Clear the current OpenVSP model


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        #==== Reset Geometry ====//
        print( "--->Resetting VSP model to blank slate\n" )
        ClearVSPModel()


    """
    return _vsp.ClearVSPModel()

@client_wrap
def InsertVSPFile(file_name, parent_geom_id):
    r"""
    Insert an external OpenVSP project into the current project. All Geoms in the external project are placed as children of the specified parent.
    If no parent or an invalid parent is given, the Geoms are inserted at the top level.
    :param [in]: file_name string *.vsp3 filename
    :param [in]: parent_geom_id string Parent geom ID (ignored with empty string)
    """
    return _vsp.InsertVSPFile(file_name, parent_geom_id)

@client_wrap
def ExportFile(*args):
    r"""
    Export a file from OpenVSP. Many formats are available, such as STL, IGES, and SVG. If a mesh is generated for a particular export,
    the ID of the MeshGeom will be returned. If no mesh is generated an empty string will be returned.


    .. code-block:: python

        wid = AddGeom( "WING" )             # Add Wing

        ExportFile( "Airfoil_Metadata.csv", SET_ALL, EXPORT_SELIG_AIRFOIL )

        mesh_id = ExportFile( "Example_Mesh.msh", SET_ALL, EXPORT_GMSH )
        DeleteGeom( mesh_id ) # Delete the mesh generated by the GMSH export


    See also: EXPORT_TYPE
    :param [in]: file_name Export file name
    :param [in]: thick_set Set index to export (i.e. SET_ALL)
    :param [in]: file_type File type enum (i.e. EXPORT_IGES)
    :param [in]: subsFlag Flag to tag subsurfaces if MeshGeom is created
    :param [in]: thin_set Set index to export as degenerate geometry (i.e. SET_NONE)
    :rtype: string
    :return: Mesh Geom ID if the export generates a mesh
    """
    return _vsp.ExportFile(*args)

@client_wrap
def ImportFile(file_name, file_type, parent):
    r"""
    Import a file into OpenVSP. Many formats are available, such as NASCART, V2, and BEM). The imported Geom, mesh, or other object is inserted
    as a child of the specified parent. If no parent or an invalid parent is given, the import will be done at the top level.
    See also: IMPORT_TYPE
    :param [in]: file_name Import file name
    :param [in]: file_type File type enum (i.e. IMPORT_PTS)
    :param [in]: parent Parent Geom ID (ignored with empty string)
    """
    return _vsp.ImportFile(file_name, file_type, parent)

@client_wrap
def SetBEMPropID(prop_id):
    r"""
    Set the ID of the propeller to be exported to a BEM file. Call this function before ExportFile.


    .. code-block:: python

        #==== Add Prop Geometry ====//
        prop_id = AddGeom( "PROP" )

        SetBEMPropID( prop_id )

        ExportFile( "ExampleBEM.bem", SET_ALL, EXPORT_BEM )


    See also: EXPORT_TYPE, ExportFile
    :param [in]: prop_id Propeller Geom ID
    """
    return _vsp.SetBEMPropID(prop_id)

@client_wrap
def ReadApplyDESFile(file_name):
    r"""
    Read in and apply a design file (*.des) to the current OpenVSP project
    :param [in]: file_name *.des input file
    """
    return _vsp.ReadApplyDESFile(file_name)

@client_wrap
def WriteDESFile(file_name):
    r"""
    Write all design variables to a design file (*.des)
    :param [in]: file_name *.des output file
    """
    return _vsp.WriteDESFile(file_name)

@client_wrap
def ReadApplyXDDMFile(file_name):
    r"""
    Read in and apply a Cart3D XDDM file (*.xddm) to the current OpenVSP project
    :param [in]: file_name *.xddm input file
    """
    return _vsp.ReadApplyXDDMFile(file_name)

@client_wrap
def WriteXDDMFile(file_name):
    r"""
    Write all design variables to a Cart3D XDDM file (*.xddm)
    :param [in]: file_name *.xddm output file
    """
    return _vsp.WriteXDDMFile(file_name)

@client_wrap
def GetNumDesignVars():
    r"""
    Get the number of design variables
    :rtype: int
    :return: int Number of design variables
    """
    return _vsp.GetNumDesignVars()

@client_wrap
def AddDesignVar(parm_id, type):
    r"""
    Add a design variable
    See also: XDDM_QUANTITY_TYPE
    :param [in]: parm_id string Parm ID
    :param [in]: type XDDM type enum (XDDM_VAR or XDDM_CONST)
    """
    return _vsp.AddDesignVar(parm_id, type)

@client_wrap
def DeleteAllDesignVars():
    r"""    Delete all design variables"""
    return _vsp.DeleteAllDesignVars()

@client_wrap
def GetDesignVar(index):
    r"""
    Get the Parm ID of the specified design variable
    :param [in]: index Index of design variable
    :rtype: string
    :return: Parm ID
    """
    return _vsp.GetDesignVar(index)

@client_wrap
def GetDesignVarType(index):
    r"""
    Get the XDDM type of the specified design variable
    See also: XDDM_QUANTITY_TYPE
    :param [in]: index Index of design variable
    :rtype: int
    :return: XDDM type enum (XDDM_VAR or XDDM_CONST)
    """
    return _vsp.GetDesignVarType(index)

@client_wrap
def SetComputationFileName(file_type, file_name):
    r"""
    Get the file name of a specified file type. Note, this function cannot be used to set FEA Mesh file names.


    .. code-block:: python

        #==== Set File Name ====//
        SetComputationFileName( DEGEN_GEOM_CSV_TYPE, "TestDegenScript.csv" )

        #==== Run Degen Geom ====//
        ComputeDegenGeom( SET_ALL, DEGEN_GEOM_CSV_TYPE )


    See also: COMPUTATION_FILE_TYPE, SetFeaMeshFileName
    :param [in]: file_type File type enum (i.e. CFD_TRI_TYPE, COMP_GEOM_TXT_TYPE)
    :param [in]: file_name File name
    """
    return _vsp.SetComputationFileName(file_type, file_name)

@client_wrap
def ComputeMassProps(set, num_slices, idir):
    r"""
    Compute mass properties for the components in the set. Alternatively can be run through the Analysis Manager with 'MassProp'.


    .. code-block:: python

        #==== Test Mass Props ====//
        pid = AddGeom( "POD", "" )

        mesh_id = ComputeMassProps( SET_ALL, 20, X_DIR )

        mass_res_id = FindLatestResultsID( "Mass_Properties" )

        double_arr = GetDoubleResults( mass_res_id, "Total_Mass" )

        if  len(double_arr) != 1 : print( "---> Error: API ComputeMassProps" )


    See also: SetAnalysisInputDefaults, PrintAnalysisInputs, ExecAnalysis
    :param [in]: set Set index (i.e. SET_ALL)
    :param [in]: num_slices Number of slices
    :param [in]: idir Direction of slicing for integration
    :rtype: string
    :return: MeshGeom ID
    """
    return _vsp.ComputeMassProps(set, num_slices, idir)

@client_wrap
def ComputeCompGeom(set, half_mesh, file_export_types):
    r"""
    Mesh, intersect, and trim components in the set. Alternatively can be run through the Analysis Manager with 'CompGeom'.


    .. code-block:: python

        #==== Add Pod Geom ====//
        pid = AddGeom( "POD", "" )

        #==== Run CompGeom And Get Results ====//
        mesh_id = ComputeCompGeom( SET_ALL, False, 0 )                      # Half Mesh false and no file export

        comp_res_id = FindLatestResultsID( "Comp_Geom" )                    # Find Results ID

        double_arr = GetDoubleResults( comp_res_id, "Wet_Area" )    # Extract Results


    See also: SetAnalysisInputDefaults, PrintAnalysisInputs, ExecAnalysis, COMPUTATION_FILE_TYPE
    :param [in]: set Set index (i.e. SET_ALL)
    :param [in]: half_mesh Flag to ignore surfaces on the negative side of the XZ plane (e.g. symmetry)
    :param [in]: file_export_types CompGeom file type to export (supports XOR i.e. COMP_GEOM_CSV_TYPE & COMP_GEOM_TXT_TYPE )
    :rtype: string
    :return: MeshGeom ID
    """
    return _vsp.ComputeCompGeom(set, half_mesh, file_export_types)

@client_wrap
def ComputePlaneSlice(set, num_slices, norm, auto_bnd, start_bnd=0, end_bnd=0, measureduct=False):
    r"""
    Slice and mesh the components in the set. Alternatively can be run through the Analysis Manager with 'PlanarSlice'.


    .. code-block:: python

        #==== Add Pod Geom ====//
        pid = AddGeom( "POD", "" )

        #==== Test Plane Slice ====//
        slice_mesh_id = ComputePlaneSlice( 0, 6, vec3d( 0.0, 0.0, 1.0 ), True )

        pslice_results = FindLatestResultsID( "Slice" )

        double_arr = GetDoubleResults( pslice_results, "Slice_Area" )

        if  len(double_arr) != 6 : print( "---> Error: API ComputePlaneSlice" )


    See also: SetAnalysisInputDefaults, PrintAnalysisInputs, ExecAnalysis
    :param [in]: set Set index (i.e. SET_ALL)
    :param [in]: num_slices Number of slices
    :param [in]: norm Normal axis for all slices
    :param [in]: auto_bnd Flag to automatically set the start and end bound locations
    :param [in]: start_bnd Location of the first slice along the normal axis (default: 0.0)
    :param [in]: end_bnd Location of the last slice along the normal axis (default: 0.0)
    :param [in]: measureduct Flag to measure negative area inside positive area (default: false)
    :rtype: string
    :return: MeshGeom ID
    """
    return _vsp.ComputePlaneSlice(set, num_slices, norm, auto_bnd, start_bnd, end_bnd, measureduct)

@client_wrap
def ComputeDegenGeom(set, file_export_types):
    r"""
    Compute the degenerate geometry representation for the components in the set. Alternatively can be run through the Analysis Manager with 'DegenGeom' or 'VSPAERODegenGeom'.


    .. code-block:: python

        #==== Set File Name ====//
        SetComputationFileName( DEGEN_GEOM_CSV_TYPE, "TestDegenScript.csv" )

        #==== Run Degen Geom ====//
        ComputeDegenGeom( SET_ALL, DEGEN_GEOM_CSV_TYPE )


    See also: SetAnalysisInputDefaults, PrintAnalysisInputs, ExecAnalysis, COMPUTATION_FILE_TYPE
    :param [in]: set int Set index (i.e. SET_ALL)
    :param [in]: file_export_types int DegenGeom file type to export (supports XOR i.e DEGEN_GEOM_M_TYPE & DEGEN_GEOM_CSV_TYPE)
    """
    return _vsp.ComputeDegenGeom(set, file_export_types)

@client_wrap
def ComputeCFDMesh(set, degenset, file_export_types):
    r"""
    Create a CFD Mesh for the components in the set. This analysis cannot be run through the Analysis Manager.


    .. code-block:: python

        #==== CFDMesh Method Facet Export =====//
        SetComputationFileName( CFD_FACET_TYPE, "TestCFDMeshFacet_API.facet" )

       print( "\tComputing CFDMesh..." )

        ComputeCFDMesh( SET_ALL, SET_NONE, CFD_FACET_TYPE )


    See also: COMPUTATION_FILE_TYPE
    :param [in]: set int Set index (i.e. SET_ALL)
    :param [in]: degenset int DegenSet index (i.e. SET_NONE)
    :param [in]: file_export_types int CFD Mesh file type to export (supports XOR i.e CFD_SRF_TYPE & CFD_STL_TYPE)
    """
    return _vsp.ComputeCFDMesh(set, degenset, file_export_types)

@client_wrap
def SetCFDMeshVal(type, val):
    r"""
    Set the value of a specific CFD Mesh option


    .. code-block:: python

        SetCFDMeshVal( CFD_MIN_EDGE_LEN, 1.0 )


    See also: CFD_CONTROL_TYPE
    :param [in]: type int CFD Mesh control type enum (i.e. CFD_GROWTH_RATIO)
    :param [in]: val double Value to set
    """
    return _vsp.SetCFDMeshVal(type, val)

@client_wrap
def SetCFDWakeFlag(geom_id, flag):
    r"""
    Activate or deactivate the CFD Mesh wake for a particular Geom. Note, the wake flag is only applicable for wing-type surfaces.
    Also, this function is simply an alternative to setting the value of the Parm with the available Parm setting API functions.


    .. code-block:: python

        #==== Add Wing Geom ====//
        wid = AddGeom( "WING", "" )

        SetCFDWakeFlag( wid, True )
        # This is equivalent to SetParmValUpdate( wid, "Wake", "Shape", 1.0 )
        # To change the scale: SetParmValUpdate( wid, "WakeScale", "WakeSettings", 10.0 )
        # To change the angle: SetParmValUpdate( wid, "WakeAngle", "WakeSettings", -5.0 )


    See also: SetParmVal, SetParmValUpdate
    :param [in]: geom_id string Geom ID
    :param [in]: flag True to activate, false to deactivate
    """
    return _vsp.SetCFDWakeFlag(geom_id, flag)

@client_wrap
def DeleteAllCFDSources():
    r"""
    Delete all CFD Mesh sources for all Geoms


    .. code-block:: python

        #==== Add Pod Geom ====//
        pid = AddGeom( "POD", "" )

        AddCFDSource( POINT_SOURCE, pid, 0, 0.25, 2.0, 0.5, 0.5 )      # Add A Point Source

        DeleteAllCFDSources()


    """
    return _vsp.DeleteAllCFDSources()

@client_wrap
def AddDefaultSources():
    r"""
    Add default CFD Mesh sources for all Geoms


    .. code-block:: python

        #==== Add Pod Geom ====//
        pid = AddGeom( "POD", "" )

        AddDefaultSources() # 3 Sources: Def_Fwd_PS, Def_Aft_PS, Def_Fwd_Aft_LS


    """
    return _vsp.AddDefaultSources()

@client_wrap
def AddCFDSource(type, geom_id, surf_index, l1, r1, u1, w1, l2=0, r2=0, u2=0, w2=0):
    r"""
    Add a CFD Mesh default source for the indicated Geom. Note, certain input params may not be used depending on the source type


    .. code-block:: python

        #==== Add Pod Geom ====//
        pid = AddGeom( "POD", "" )

        AddCFDSource( POINT_SOURCE, pid, 0, 0.25, 2.0, 0.5, 0.5 )      # Add A Point Source


    See also: CFD_MESH_SOURCE_TYPE
    :param [in]: type CFD Mesh source type( i.e.BOX_SOURCE )
    :param [in]: geom_id string Geom ID
    :param [in]: surf_index Main surface index
    :param [in]: l1 Source first edge length
    :param [in]: r1 Source first radius
    :param [in]: u1 Source first U location
    :param [in]: w1 Source first W location
    :param [in]: l2 Source second edge length
    :param [in]: r2 Source second radius
    :param [in]: u2 Source second U location
    :param [in]: w2 Source second W location
    """
    return _vsp.AddCFDSource(type, geom_id, surf_index, l1, r1, u1, w1, l2, r2, u2, w2)

@client_wrap
def GetVSPAERORefWingID():
    r"""
    Get ID of the current VSPAERO reference Geom
    :rtype: string
    :return: Reference Geom ID
    """
    return _vsp.GetVSPAERORefWingID()

@client_wrap
def SetVSPAERORefWingID(geom_id):
    r"""
    Set the current VSPAERO reference Geom ID


    .. code-block:: python

        #==== Add Wing Geom and set some parameters =====//
        wing_id = AddGeom( "WING" )

        SetGeomName( wing_id, "MainWing" )

        #==== Add Vertical tail and set some parameters =====//
        vert_id = AddGeom( "WING" )

        SetGeomName( vert_id, "Vert" )

        SetParmValUpdate( vert_id, "TotalArea", "WingGeom", 10.0 )
        SetParmValUpdate( vert_id, "X_Rel_Location", "XForm", 8.5 )
        SetParmValUpdate( vert_id, "X_Rel_Rotation", "XForm", 90 )

        #==== Set VSPAERO Reference lengths & areas ====//
        SetVSPAERORefWingID( wing_id ) # Set as reference wing for VSPAERO

        print( "VSPAERO Reference Wing ID: ", False )

        print( GetVSPAERORefWingID() )


    :param [in]: geom_id Reference Geom ID
    """
    return _vsp.SetVSPAERORefWingID(geom_id)

@client_wrap
def GetNumAnalysis():
    r"""
    Get the number of analysis types available in the Analysis Manager


    .. code-block:: python

        nanalysis = GetNumAnalysis()

        print( f"Number of registered analyses: {nanalysis}" )


    :rtype: int
    :return: Number of analyses
    """
    return _vsp.GetNumAnalysis()

@client_wrap
def ListAnalysis():
    r"""
    Get the name of every available analysis in the Analysis Manager


    .. code-block:: python

        analysis_array = ListAnalysis()

        print( "List of Available Analyses: " )

        for i in range(int( len(analysis_array) )):

            print( "    " + analysis_array[i] )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of analysis names
    """
    return _vsp.ListAnalysis()

@client_wrap
def GetAnalysisInputNames(analysis):
    r"""
    Get the name of every available input for a particular analysis


    .. code-block:: python

        analysis_name = "VSPAEROComputeGeometry"

        in_names =  GetAnalysisInputNames( analysis_name )

        print("Analysis Inputs: ")

        for i in range(int( len(in_names) )):

            print( ( "\t" + in_names[i] + "\n" ) )


    :param [in]: analysis Analysis name
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of input names
    """
    return _vsp.GetAnalysisInputNames(analysis)

@client_wrap
def GetAnalysisDoc(analysis):
    r"""
    Get the analysis documentation string


    .. code-block:: python

        analysis_name = "VSPAEROComputeGeometry"

        doc = GetAnalysisDoc( analysis_name )


    :param [in]: analysis Analysis name
    :rtype: string
    :return: Documentation string
    """
    return _vsp.GetAnalysisDoc(analysis)

@client_wrap
def GetAnalysisInputDoc(analysis, name):
    r"""
    Get the documentation string for the particular analysis and input




    :param [in]: analysis Analysis name
    :param [in]: name Input name
    :rtype: string
    :return: Documentation string
    """
    return _vsp.GetAnalysisInputDoc(analysis, name)

@client_wrap
def ExecAnalysis(analysis):
    r"""
    Execute an analysis through the Analysis Manager


    .. code-block:: python

        analysis_name = "VSPAEROComputeGeometry"

        res_id = ExecAnalysis( analysis_name )


    :param [in]: analysis Analysis name
    :rtype: string
    :return: Result ID
    """
    return _vsp.ExecAnalysis(analysis)

@client_wrap
def GetNumAnalysisInputData(analysis, name):
    r"""
    Get the documentation string for the particular analysis and input
    :param [in]: analysis Analysis name
    :param [in]: name Input name
    :rtype: int
    :return: Documentation string
    """
    return _vsp.GetNumAnalysisInputData(analysis, name)

@client_wrap
def GetAnalysisInputType(analysis, name):
    r"""
    Get the data type for a particulat analysis type and input


    .. code-block:: python

        analysis = "VSPAEROComputeGeometry"

        inp_array = GetAnalysisInputNames( analysis )

        for j in range(int( len(inp_array) )):

            typ = GetAnalysisInputType( analysis, inp_array[j] )


    See also: RES_DATA_TYPE
    :param [in]: analysis Analysis name
    :param [in]: name Input name
    :rtype: int
    :return: int Data type enum (i.e. DOUBLE_DATA)
    """
    return _vsp.GetAnalysisInputType(analysis, name)

@client_wrap
def GetIntAnalysisInput(analysis, name, index=0):
    r"""
    Get the current integer values for the particular analysis, input, and data index


    .. code-block:: python

        #==== Analysis: VSPAero Compute Geometry ====//
        analysis_name = "VSPAEROComputeGeometry"

        # Set to panel method
        analysis_method = GetIntAnalysisInput( analysis_name, "AnalysisMethod" )

        analysis_method = [VORTEX_LATTICE]

        SetIntAnalysisInput( analysis_name, "AnalysisMethod", analysis_method )


    See also: RES_DATA_TYPE, SetIntAnalysisInput
    :param [in]: analysis string Analysis name
    :param [in]: name string Input name
    :param [in]: index int Data index
    :rtype: std::vector< int,std::allocator< int > >
    :return: vector<int> Array of analysis input values
    """
    return _vsp.GetIntAnalysisInput(analysis, name, index)

@client_wrap
def GetDoubleAnalysisInput(analysis, name, index=0):
    r"""
    Get the current double values for the particular analysis, input, and data index


    .. code-block:: python

        vinfFCinput = list( GetDoubleAnalysisInput( "ParasiteDrag", "Vinf" ) )

        vinfFCinput[0] = 629

        SetDoubleAnalysisInput( "ParasiteDrag", "Vinf", vinfFCinput )


    See also: RES_DATA_TYPE, SetDoubleAnalysisInput
    :param [in]: analysis string Analysis name
    :param [in]: name string Input name
    :param [in]: index int Data index
    :rtype: std::vector< double,std::allocator< double > >
    :return: vector<double> Array of analysis input values
    """
    return _vsp.GetDoubleAnalysisInput(analysis, name, index)

@client_wrap
def GetStringAnalysisInput(analysis, name, index=0):
    r"""
    Get the current string values for the particular analysis, input, and data index


    .. code-block:: python

        fileNameInput = GetStringAnalysisInput( "ParasiteDrag", "FileName" )

        fileNameInput = ["ParasiteDragExample"]

        SetStringAnalysisInput( "ParasiteDrag", "FileName", fileNameInput )


    See also: RES_DATA_TYPE, SetStringAnalysisInput
    :param [in]: analysis string Analysis name
    :param [in]: name string Input name
    :param [in]: index int Data index
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: vector<string> Array of analysis input values
    """
    return _vsp.GetStringAnalysisInput(analysis, name, index)

@client_wrap
def GetVec3dAnalysisInput(analysis, name, index=0):
    r"""
    Get the current vec3d values for the particular analysis, input, and data index


    .. code-block:: python

        # PlanarSlice
        norm = GetVec3dAnalysisInput( "PlanarSlice", "Norm" )

        norm[0].set_xyz( 0.23, 0.6, 0.15 )

        SetVec3dAnalysisInput( "PlanarSlice", "Norm", norm )


    See also: RES_DATA_TYPE, SetVec3dAnalysisInput
    :param [in]: analysis string Analysis name
    :param [in]: name string Input name
    :param [in]: index int Data index
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> Array of analysis input values
    """
    return _vsp.GetVec3dAnalysisInput(analysis, name, index)

@client_wrap
def SetAnalysisInputDefaults(analysis):
    r"""
    Set all input values to their defaults for a specific analysis


     .. code-block:: python

         #==== Analysis: VSPAero Compute Geometry ====//
         analysis_name = "VSPAEROComputeGeometry"

         # Set defaults
         SetAnalysisInputDefaults( analysis_name )


     :param [in]: analysis Analysis name
    """
    return _vsp.SetAnalysisInputDefaults(analysis)

@client_wrap
def SetIntAnalysisInput(analysis, name, indata, index=0):
    r"""
    Set the value of a particular analysis input of integer type


    .. code-block:: python

        #==== Analysis: VSPAero Compute Geometry ====//
        analysis_name = "VSPAEROComputeGeometry"

        # Set to panel method
        analysis_method = GetIntAnalysisInput( analysis_name, "AnalysisMethod" )

        analysis_method = [VORTEX_LATTICE]

        SetIntAnalysisInput( analysis_name, "AnalysisMethod", analysis_method )


    See also: GetIntAnalysisInput
    :param [in]: analysis string Analysis name
    :param [in]: name string Input name
    :param [in]: indata vector<int> Array of integer values to set the input to
    :param [in]: index int Data index
    """
    return _vsp.SetIntAnalysisInput(analysis, name, indata, index)

@client_wrap
def SetDoubleAnalysisInput(analysis, name, indata, index=0):
    r"""
    Set the value of a particular analysis input of double type


    .. code-block:: python

        #==== Analysis: CpSlicer ====//
        analysis_name = "CpSlicer"

        # Setup cuts
        ycuts = []
        ycuts.append( 2.0 )
        ycuts.append( 4.5 )
        ycuts.append( 8.0 )

        SetDoubleAnalysisInput( analysis_name, "YSlicePosVec", ycuts, 0 )


    See also: GetDoubleAnalysisInput
    :param [in]: analysis string Analysis name
    :param [in]: name string Input name
    :param [in]: indata vector<double> Array of double values to set the input to
    :param [in]: index int Data index
    """
    return _vsp.SetDoubleAnalysisInput(analysis, name, indata, index)

@client_wrap
def SetStringAnalysisInput(analysis, name, indata, index=0):
    r"""
    Set the value of a particular analysis input of string type


    .. code-block:: python

        fileNameInput = GetStringAnalysisInput( "ParasiteDrag", "FileName" )

        fileNameInput = ["ParasiteDragExample"]

        SetStringAnalysisInput( "ParasiteDrag", "FileName", fileNameInput )


    See also: GetStringAnalysisInput
    :param [in]: analysis string Analysis name
    :param [in]: name string Input name
    :param [in]: indata vector<string> Array of string values to set the input to
    :param [in]: index int Data index
    """
    return _vsp.SetStringAnalysisInput(analysis, name, indata, index)

@client_wrap
def SetVec3dAnalysisInput(analysis, name, indata, index=0):
    r"""
    Set the value of a particular analysis input of vec3d type


    .. code-block:: python

        # PlanarSlice
        norm = GetVec3dAnalysisInput( "PlanarSlice", "Norm" )

        norm[0].set_xyz( 0.23, 0.6, 0.15 )

        SetVec3dAnalysisInput( "PlanarSlice", "Norm", norm )


    See also: GetVec3dAnalysisInput
    :param [in]: analysis string Analysis name
    :param [in]: name string Input name
    :param [in]: indata vector<vec3d> Array of vec3d values to set the input to
    :param [in]: index int Data index
    """
    return _vsp.SetVec3dAnalysisInput(analysis, name, indata, index)

@client_wrap
def PrintAnalysisInputs(analysis_name):
    r"""
    Print to stdout all current input values for a specific analysis


    .. code-block:: python

        #==== Analysis: VSPAero Compute Geometry ====//
        analysis_name = "VSPAEROComputeGeometry"

        # list inputs, type, and current values
        PrintAnalysisInputs( analysis_name )


    :param [in]: analysis_name string Name of analysis
    """
    return _vsp.PrintAnalysisInputs(analysis_name)

@client_wrap
def PrintAnalysisDocs(analysis_name):
    r"""
    Print to stdout all current input documentation for a specific analysis


    .. code-block:: python

        #==== Analysis: VSPAero Compute Geometry ====//
        analysis_name = "VSPAEROComputeGeometry"

        # list inputs, type, and documentation
        PrintAnalysisDocs( analysis_name )


    :param [in]: analysis_name string Name of analysis
    """
    return _vsp.PrintAnalysisDocs(analysis_name)

@client_wrap
def GetAllResultsNames():
    r"""
    Get the name of all results in the Results Manager


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        results_array = GetAllResultsNames()

        for i in range(int( len(results_array) )):

            resid = FindLatestResultsID( results_array[i] )
            PrintResults( resid )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of result names
    """
    return _vsp.GetAllResultsNames()

@client_wrap
def GetAllDataNames(results_id):
    r"""
    Get all data names for a particular result


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        res_id = FindResultsID( "Test_Results" )

        data_names = GetAllDataNames( res_id )

        if  len(data_names) != 5 : print( "---> Error: API GetAllDataNames" )


    :param [in]: results_id Result ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of result names
    """
    return _vsp.GetAllDataNames(results_id)

@client_wrap
def GetNumResults(name):
    r"""
    Get the number of results for a particular result name


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        if ( GetNumResults( "Test_Results" ) != 2 ): print( "---> Error: API GetNumResults" )


    :param [in]: name Input name
    :rtype: int
    :return: Number of results
    """
    return _vsp.GetNumResults(name)

@client_wrap
def GetResultsName(results_id):
    r"""
    Get the name of a result given its ID


    .. code-block:: python

        #==== Analysis: VSPAero Compute Geometry ====//
        analysis_name = "VSPAEROComputeGeometry"

        # Set defaults
        SetAnalysisInputDefaults( analysis_name )

        res_id = ( ExecAnalysis( analysis_name ) )

        print( "Results Name: ", False )

        print( GetResultsName( res_id ) )


    :param [in]: results_id Result ID
    :rtype: string
    :return: Result name
    """
    return _vsp.GetResultsName(results_id)

@client_wrap
def GetResultsSetDoc(results_id):
    r"""
    Get the documentation string for a result given its ID


    .. code-block:: python

        #==== Analysis: VSPAero Compute Geometry ====//
        analysis_name = "VSPAEROComputeGeometry"

        # Set defaults
        SetAnalysisInputDefaults( analysis_name )

        res_id = ( ExecAnalysis( analysis_name ) )

        print( "Results doc: ", False )

        print( GetResultsSetDoc( res_id ) )


    :param [in]: results_id Result ID
    :rtype: string
    :return: Result documentation string
    """
    return _vsp.GetResultsSetDoc(results_id)

@client_wrap
def GetResultsEntryDoc(results_id, data_name):
    r"""GetResultsEntryDoc(std::string const & results_id, std::string const & data_name) -> std::string"""
    return _vsp.GetResultsEntryDoc(results_id, data_name)

@client_wrap
def FindResultsID(name, index=0):
    r"""
    Find a results ID given its name and index


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        res_id = FindResultsID( "Test_Results" )

        if  len(res_id) == 0 : print( "---> Error: API FindResultsID" )


    :param [in]: name Result name
    :param [in]: index Result index
    :rtype: string
    :return: Result ID
    """
    return _vsp.FindResultsID(name, index)

@client_wrap
def FindLatestResultsID(name):
    r"""
    Find the latest results ID for particular result name


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        results_array = GetAllResultsNames()

        for i in range(int( len(results_array) )):

            resid = FindLatestResultsID( results_array[i] )
            PrintResults( resid )


    :param [in]: name Result name
    :rtype: string
    :return: Result ID
    """
    return _vsp.FindLatestResultsID(name)

@client_wrap
def GetNumData(results_id, data_name):
    r"""
    Get the number of data values for a given result ID and data name


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        res_id = FindResultsID( "Test_Results" )

        if ( GetNumData( res_id, "Test_Int" ) != 2 ): print( "---> Error: API GetNumData " )

        int_arr = GetIntResults( res_id, "Test_Int", 0 )

        if  int_arr[0] != 1 : print( "---> Error: API GetIntResults" )

        int_arr = GetIntResults( res_id, "Test_Int", 1 )

        if  int_arr[0] != 2 : print( "---> Error: API GetIntResults" )


    :param [in]: results_id Result ID
    :param [in]: data_name Data name
    :rtype: int
    :return: Number of data values
    """
    return _vsp.GetNumData(results_id, data_name)

@client_wrap
def GetResultsType(results_id, data_name):
    r"""
    Get the data type for a given result ID and data name


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        res_id = FindResultsID( "Test_Results" )

        res_array = GetAllDataNames( res_id )

        for j in range(int( len(res_array) )):

            typ = GetResultsType( res_id, res_array[j] )


    See also: RES_DATA_TYPE
    :param [in]: results_id Result ID
    :param [in]: data_name Data name
    :rtype: int
    :return: Data type enum (i.e. DOUBLE_DATA)
    """
    return _vsp.GetResultsType(results_id, data_name)

@client_wrap
def GetIntResults(id, name, index=0):
    r"""
    Get all integer values for a particular result, name, and index


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        res_id = FindResultsID( "Test_Results" )

        if ( GetNumData( res_id, "Test_Int" ) != 2 ): print( "---> Error: API GetNumData " )

        int_arr = GetIntResults( res_id, "Test_Int", 0 )

        if  int_arr[0] != 1 : print( "---> Error: API GetIntResults" )

        int_arr = GetIntResults( res_id, "Test_Int", 1 )

        if  int_arr[0] != 2 : print( "---> Error: API GetIntResults" )


    :param [in]: id Result ID
    :param [in]: name Data name
    :param [in]: index Data index
    :rtype: std::vector< int,std::allocator< int > >
    :return: Array of data values
    """
    return _vsp.GetIntResults(id, name, index)

@client_wrap
def GetDoubleResults(id, name, index=0):
    r"""
    Get all double values for a particular result, name, and index


    .. code-block:: python

        #==== Add Pod Geom ====//
        pid = AddGeom( "POD", "" )

        #==== Run CompGeom And View Results ====//
        mesh_id = ComputeCompGeom( SET_ALL, False, 0 )                      # Half Mesh false and no file export

        comp_res_id = FindLatestResultsID( "Comp_Geom" )                    # Find Results ID

        double_arr = GetDoubleResults( comp_res_id, "Wet_Area" )    # Extract Results


    :param [in]: id Result ID
    :param [in]: name Data name
    :param [in]: index Data index
    :rtype: std::vector< double,std::allocator< double > >
    :return: Array of data values
    """
    return _vsp.GetDoubleResults(id, name, index)

@client_wrap
def GetDoubleMatResults(id, name, index=0):
    r"""
    Get all matrix (vector<vector<double>>) values for a particular result, name, and index
    :param [in]: id Result ID
    :param [in]: name Data name
    :param [in]: index Data index
    :rtype: std::vector< std::vector< double,std::allocator< double > >,std::allocator< std::vector< double,std::allocator< double > > > >
    :return: 2D array of data values
    """
    return _vsp.GetDoubleMatResults(id, name, index)

@client_wrap
def GetStringResults(id, name, index=0):
    r"""
    Get all string values for a particular result, name, and index


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        res_id = FindResultsID( "Test_Results" )

        str_arr = GetStringResults( res_id, "Test_String" )

        if ( str_arr[0] != "This Is A Test" ): print( "---> Error: API GetStringResults" )


    :param [in]: id Result ID
    :param [in]: name Data name
    :param [in]: index Data index
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of data values
    """
    return _vsp.GetStringResults(id, name, index)

@client_wrap
def GetVec3dResults(id, name, index=0):
    r"""
    Get all vec3d values for a particular result, name, and index


    .. code-block:: python

        #==== Write Some Fake Test Results =====//

        tol = 0.00001

        WriteTestResults()

        res_id = FindLatestResultsID( "Test_Results" )

        vec3d_vec = GetVec3dResults( res_id, "Test_Vec3d" )

        print( "X: ", False )
        print( vec3d_vec[0].x(), False )

        print( "\tY: ", False )
        print( vec3d_vec[0].y(), False )

        print( "\tZ: ", False )
        print( vec3d_vec[0].z() )


    :param [in]: id Result ID
    :param [in]: name Data name
    :param [in]: index Data index
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: Array of data values
    """
    return _vsp.GetVec3dResults(id, name, index)

@client_wrap
def CreateGeomResults(geom_id, name):
    r"""
    Create a new result for a Geom


    .. code-block:: python

        #==== Test Comp Geom ====//
        gid1 = AddGeom( "POD", "" )

        mesh_id = ComputeCompGeom( 0, False, 0 )

        #==== Test Comp Geom Mesh Results ====//
        mesh_geom_res_id = CreateGeomResults( mesh_id, "Comp_Mesh" )

        int_arr = GetIntResults( mesh_geom_res_id, "Num_Tris" )

        if  int_arr[0] < 4 : print( "---> Error: API CreateGeomResults" )


    :param [in]: geom_id string Geom ID
    :param [in]: name Result name
    :rtype: string
    :return: Result ID
    """
    return _vsp.CreateGeomResults(geom_id, name)

@client_wrap
def DeleteAllResults():
    r"""
    Delete all results


    .. code-block:: python

        #==== Test Comp Geom ====//
        gid1 = AddGeom( "POD", "" )

        mesh_id = ComputeCompGeom( 0, False, 0 )

        #==== Test Comp Geom Mesh Results ====//
        mesh_geom_res_id = CreateGeomResults( mesh_id, "Comp_Mesh" )

        DeleteAllResults()

        if ( GetNumResults( "Comp_Mesh" ) != 0 ): print( "---> Error: API DeleteAllResults" )


    """
    return _vsp.DeleteAllResults()

@client_wrap
def DeleteResult(id):
    r"""
    Delete a particular result


    .. code-block:: python

        #==== Test Comp Geom ====//
        gid1 = AddGeom( "POD", "" )

        mesh_id = ComputeCompGeom( 0, False, 0 )

        #==== Test Comp Geom Mesh Results ====//
        mesh_geom_res_id = CreateGeomResults( mesh_id, "Comp_Mesh" )

        DeleteResult( mesh_geom_res_id )

        if ( GetNumResults( "Comp_Mesh" ) != 0 ): print( "---> Error: API DeleteResult" )


    :param [in]: id Result ID
    """
    return _vsp.DeleteResult(id)

@client_wrap
def WriteResultsCSVFile(id, file_name):
    r"""
    Export a result to CSV


    .. code-block:: python

        # Add Pod Geom
        pid = AddGeom( "POD" )

        analysis_name = "VSPAEROComputeGeometry"

        rid = ExecAnalysis( analysis_name )

        WriteResultsCSVFile( rid, "CompGeomRes.csv" )


    :param [in]: id Rsult ID
    :param [in]: file_name CSV output file name
    """
    return _vsp.WriteResultsCSVFile(id, file_name)

@client_wrap
def PrintResults(results_id):
    r"""
    Print a result's name value pairs to stdout


    .. code-block:: python

        # Add Pod Geom
        pid = AddGeom( "POD" )

        analysis_name = "VSPAEROComputeGeometry"

        rid = ExecAnalysis( analysis_name )

        # Get & Display Results
        PrintResults( rid )


    :param [in]: results_id string Result ID
    """
    return _vsp.PrintResults(results_id)

@client_wrap
def PrintResultsDocs(results_id):
    r"""
    Print a result's names and documentation to stdout


    .. code-block:: python

        # Add Pod Geom
        pid = AddGeom( "POD" )

        analysis_name = "VSPAEROComputeGeometry"

        rid = ExecAnalysis( analysis_name )

        # Get & Display Results Docs
        PrintResultsDocs( rid )


    :param [in]: results_id string Result ID
    """
    return _vsp.PrintResultsDocs(results_id)

@client_wrap
def WriteTestResults():
    r"""
    Generate some example results for testing.


    .. code-block:: python

        #==== Write Some Fake Test Results =====//
        WriteTestResults()

        results_array = GetAllResultsNames()

        for i in range( len( results_array ) ):
            resid = FindLatestResultsID( results_array[i] )
            PrintResults( resid )


    """
    return _vsp.WriteTestResults()

@client_wrap
def InitGUI():
    r"""
    Initialize the GUI so it can be called from the API.  Must be called before other GUI related API calls.
    In a multi-threaded environment, this must be called from the main thread only.


    .. code-block:: python


        InitGUI()
        StartGUI()



    See also: StartGUI
    """
    return _vsp.InitGUI()

@client_wrap
def StartGUI():
    r"""
    Launch the interactive OpenVSP GUI.  In a multi-threaded environment, this must be called from the main thread only.
    This starts the GUI event loop.  It will also show the main screen and screens displayed when StopGUI() was
    previously called.


    .. code-block:: python


        InitGUI()
        StartGUI()



    See also: InitGUI
    """
    return _vsp.StartGUI()

@client_wrap
def EnableStopGUIMenuItem():
    r"""
    Enable Stop GUI Menu Item from the OpenVSP GUI.

    Typically used for the blocking-mode OpenVSP GUI from the API.

    This will add a "Stop GUI" option to the file pulldown menu and will also cause the exit button on the
    window frame to have the same effect.  When selected, these options will stop the OpenVSP GUI event loop,
    returning control to the API program.  OpenVSP will not terminate, the model will remain in memory and will
    be responsive to subsequent API calls.



    .. code-block:: python


        InitGUI()
        EnableStopGUIMenuItem()
        StartGUI()



    See also: InitGUI, DisableStopGUIMenuItem
    """
    return _vsp.EnableStopGUIMenuItem()

@client_wrap
def DisableStopGUIMenuItem():
    r"""
    Disable Stop GUI Menu Item from the OpenVSP GUI.

    This reverses the operation of EnableStopGUIMenuItem.



    .. code-block:: python


        InitGUI()
        EnableStopGUIMenuItem()
        DisableStopGUIMenuItem()
        StartGUI()



    See also: InitGUI, EnableStopGUIMenuItem
    """
    return _vsp.DisableStopGUIMenuItem()

@client_wrap
def StopGUI():
    r"""
    Stop OpenVSP GUI event loop and hide screens.  Keep OpenVSP running and in memory.


    .. code-block:: python


        InitGUI()
        StartGUI()

        StopGUI()

        StartGUI()



    See also: InitGUI, StartGUI
    """
    return _vsp.StopGUI()

@client_wrap
def PopupMsg(msg):
    r"""
    Cause OpenVSP to display a popup message.


    .. code-block:: python


        InitGUI()
        StartGUI()

        PopupMsg( "This is a popup message." )



    :param [in]: msg string Message to display.
    """
    return _vsp.PopupMsg(msg)

@client_wrap
def UpdateGUI():
    r"""
    Tell OpenVSP that the GUI needs to be updated.


    .. code-block:: python


        InitGUI()
        StartGUI()

        pod_id = AddGeom( "POD" )

        length = FindParm( pod_id, "Length", "Design" )

        SetParmVal( length, 13.0 )

        UpdateGUI()



    See also: InitGUI, StartGUI
    """
    return _vsp.UpdateGUI()

@client_wrap
def IsGUIBuild():
    r"""
    Test if the current OpenVSP build includes graphics capabilities.


    .. code-block:: python


        if ( IsGUIBuild() ):
            print( "OpenVSP build is graphics capable." )
        else:
            print( "OpenVSP build is not graphics capable." )



    :rtype: boolean
    :return: bool True if the current OpenVSP build includes graphics capabilities.  False otherwise.
    """
    return _vsp.IsGUIBuild()

@client_wrap
def Lock():
    r"""
    Obtain the lock on the OpenVSP GUI event loop.  This will prevent the interactive GUI from
    updating or accepting user input until the lock is released -- thereby allowing longer-time
    commands including analyses to execute without the chance of the OpenVSP state changing during
    execution.



    .. code-block:: python


        InitGUI()
        StartGUI()

        pod_id = AddGeom( "POD" )

        Lock()
        rid = ExecAnalysis( "CompGeom" )

        mesh_id_vec = GetStringResults( rid, "Mesh_GeomID" )

        DeleteGeomVec( mesh_id_vec )
        Unlock()



    See also: Unlock
    """
    return _vsp.Lock()

@client_wrap
def Unlock():
    r"""
    Release the lock on the OpenVSP GUI event loop.



    .. code-block:: python


        InitGUI()
        StartGUI()

        pod_id = AddGeom( "POD" )

        Lock()
        rid = ExecAnalysis( "CompGeom" )

        mesh_id_vec = GetStringResults( rid, "Mesh_GeomID" )

        DeleteGeomVec( mesh_id_vec )
        Unlock()



    See also: Lock
    """
    return _vsp.Unlock()

@client_wrap
def ScreenGrab(fname, w, h, transparentBG, autocrop=False):
    r"""
    Capture the specified screen and save to file. Note, VSP_USE_FLTK must be defined


    .. code-block:: python

        screenw = 2000                                             # Set screenshot width and height
        screenh = 2000

        fname = "test_screen_grab.png"

        ScreenGrab( fname, screenw, screenh, True, True )                # Take PNG screenshot


    :param [in]: fname string Output file name
    :param [in]: w int Width of screen grab
    :param [in]: h int Height of screen grab
    :param [in]: transparentBG bool Transparent background flag
    :param [in]: autocrop bool Automatically crop transparent background flag
    """
    return _vsp.ScreenGrab(fname, w, h, transparentBG, autocrop)

@client_wrap
def SetViewAxis(vaxis):
    r"""
    Toggle viewing the axis


    .. code-block:: python

        SetViewAxis( False )                                           # Turn off axis marker in corner of viewscreen


    :param [in]: vaxis True to show the axis, false to hide the axis
    """
    return _vsp.SetViewAxis(vaxis)

@client_wrap
def SetShowBorders(brdr):
    r"""
    Toggle viewing the border frame


    .. code-block:: python

        SetShowBorders( False )                                        # Turn off red/black border on active window


    :param [in]: brdr True to show the border frame, false to hide the border frame
    """
    return _vsp.SetShowBorders(brdr)

@client_wrap
def SetGeomDrawType(geom_id, type):
    r"""
    Set the draw type of the specified goemetry


    .. code-block:: python

        pid = AddGeom( "POD", "" )                             # Add Pod for testing

        SetGeomDrawType( pid, GEOM_DRAW_SHADE )                       # Make pod appear as shaded


    See also: DRAW_TYPE
    :param [in]: geom_id string Geom ID
    :param [in]: type Draw type enum (i.e. GEOM_DRAW_SHADE)
    """
    return _vsp.SetGeomDrawType(geom_id, type)

@client_wrap
def SetGeomDisplayType(geom_id, type):
    r"""
    Set the display type of the specified goemetry


    .. code-block:: python

        pid = AddGeom( "POD" )                             # Add Pod for testing

        SetGeomDisplayType( pid, DISPLAY_DEGEN_PLATE )                       # Make pod appear as Bezier plate (Degen Geom)


    See also: DISPLAY_TYPE
    :param [in]: geom_id string Geom ID
    :param [in]: type Display type enum (i.e. DISPLAY_BEZIER)
    """
    return _vsp.SetGeomDisplayType(geom_id, type)

@client_wrap
def SetBackground(r, g, b):
    r"""
    Set the background color


    .. code-block:: python

        SetBackground( 1.0, 1.0, 1.0 )                                 # Set background to bright white


    :param [in]: r Red 8-bit unsigned integer (range: 0-255)
    :param [in]: g Green 8-bit unsigned integer (range: 0-255)
    :param [in]: b Blue 8-bit unsigned integer (range: 0-255)
    """
    return _vsp.SetBackground(r, g, b)

@client_wrap
def SetGUIElementDisable(e, state):
    r"""
    Set whether all instances of GUI device type are disabled


    .. code-block:: python

        SetGUIElementDisable( GDEV_INPUT, True )

    :param [in]: e int GDEV enum for GUI device type
    :param [in]: state bool True to disable GUI device type
    """
    return _vsp.SetGUIElementDisable(e, state)

@client_wrap
def SetGUIScreenDisable(s, state):
    r"""
    Set whether screen is disabled


    .. code-block:: python

        SetGUIScreenDisable( VSP_CFD_MESH_SCREEN, True )

    :param [in]: e int GUI_VSP_SCREEN enum for screen
    :param [in]: state bool True to disable screen
    """
    return _vsp.SetGUIScreenDisable(s, state)

@client_wrap
def SetGeomScreenDisable(s, state):
    r"""
    Set whether geom screen is disabled


    .. code-block:: python

        SetGeomScreenDisable( ALL_GEOM_SCREENS, True )

    :param [in]: e int GUI_GEOM_SCREEN enum for geom screen
    :param [in]: state bool True to disable geom screen
    """
    return _vsp.SetGeomScreenDisable(s, state)

@client_wrap
def GetGeomTypes():
    r"""
    Get an array of all Geom types (i.e FUSELAGE, POD, etc.)


    .. code-block:: python

        #==== Add Pod Geometries ====//
        pod1 = AddGeom( "POD", "" )
        pod2 = AddGeom( "POD", "" )

        type_array = GetGeomTypes()

        if ( type_array[0] != "POD" ): print( "---> Error: API GetGeomTypes  " )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Geom type names
    """
    return _vsp.GetGeomTypes()

@client_wrap
def AddGeom(*args):
    r"""
    Add a new Geom of given type as a child of the specified parent. If no parent or an invalid parent is given, the Geom is placed at the top level


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )


    :param [in]: type Geom type (i.e FUSELAGE, POD, etc.)
    :param [in]: parent Parent Geom ID
    :rtype: string
    :return: Geom ID
    """
    return _vsp.AddGeom(*args)

@client_wrap
def UpdateGeom(geom_id):
    r"""
    Perform an update for the specified Geom


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        SetParmVal( pod_id, "X_Rel_Location", "XForm", 5.0 )

        UpdateGeom( pod_id ) # Faster than updating the whole vehicle


    See also: Update()
    :param [in]: geom_id string Geom ID
    """
    return _vsp.UpdateGeom(geom_id)

@client_wrap
def DeleteGeom(geom_id):
    r"""
    Delete a particular Geom


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        DeleteGeom( wing_id )


    :param [in]: geom_id string Geom ID
    """
    return _vsp.DeleteGeom(geom_id)

@client_wrap
def DeleteGeomVec(del_vec):
    r"""
    Delete multiple Geoms


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD", "" )

        rid = ExecAnalysis( "CompGeom" )

        mesh_id_vec = GetStringResults( rid, "Mesh_GeomID" )

        DeleteGeomVec( mesh_id_vec )


    :param [in]: del_vec vector<string> Vector of Geom IDs
    """
    return _vsp.DeleteGeomVec(del_vec)

@client_wrap
def CutGeomToClipboard(geom_id):
    r"""
    Cut Geom from current location and store on clipboard


    .. code-block:: python

        #==== Add Pod Geometries ====//
        pid1 = AddGeom( "POD", "" )
        pid2 = AddGeom( "POD", "" )

        CutGeomToClipboard( pid1 )

        PasteGeomClipboard( pid2 ) # Paste Pod 1 as child of Pod 2

        geom_ids = FindGeoms()

        if  len(geom_ids) != 2 : print( "---> Error: API Cut/Paste Geom  " )


    See also: PasteGeomClipboard
    :param [in]: geom_id string Geom ID
    """
    return _vsp.CutGeomToClipboard(geom_id)

@client_wrap
def CopyGeomToClipboard(geom_id):
    r"""
    Copy Geom from current location and store on clipboard


    .. code-block:: python

        #==== Add Pod Geometries ====//
        pid1 = AddGeom( "POD", "" )
        pid2 = AddGeom( "POD", "" )

        CopyGeomToClipboard( pid1 )

        PasteGeomClipboard( pid2 ) # Paste Pod 1 as child of Pod 2

        geom_ids = FindGeoms()

        if  len(geom_ids) != 3 : print( "---> Error: API Copy/Paste Geom  " )


    See also: PasteGeomClipboard
    :param [in]: geom_id string Geom ID
    """
    return _vsp.CopyGeomToClipboard(geom_id)

@client_wrap
def PasteGeomClipboard(*args):
    r"""
    Paste Geom from clipboard into the model. The Geom is pasted as a child of the specified parent, but will be placed at top level if no parent or an invalid one is provided.


    .. code-block:: python

        #==== Add Pod Geometries ====//
        pid1 = AddGeom( "POD", "" )
        pid2 = AddGeom( "POD", "" )

        CutGeomToClipboard( pid1 )

        PasteGeomClipboard( pid2 ) # Paste Pod 1 as child of Pod 2

        geom_ids = FindGeoms()

        if  len(geom_ids) != 2 : print( "---> Error: API Cut/Paste Geom  " )


    :param [in]: parent string Parent Geom ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: vector<string> Vector of pasted Geom IDs
    """
    return _vsp.PasteGeomClipboard(*args)

@client_wrap
def FindGeoms():
    r"""
    Find and return all Geom IDs in the model


    .. code-block:: python

        #==== Add Pod Geometries ====//
        pod1 = AddGeom( "POD", "" )
        pod2 = AddGeom( "POD", "" )

        #==== There Should Be Two Geoms =====//
        geom_ids = FindGeoms()

        if  len(geom_ids) != 2 : print( "---> Error: API FindGeoms " )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of all Geom IDs
    """
    return _vsp.FindGeoms()

@client_wrap
def FindGeomsWithName(name):
    r"""
    Find and return all Geom IDs with the specified name


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD", "" )

        SetGeomName( pid, "ExamplePodName" )

        geom_ids = FindGeomsWithName( "ExamplePodName" )

        if  len(geom_ids) != 1 :
            print( "---> Error: API FindGeomsWithName " )


    See also: FindGeom
    :param [in]: name Geom name
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Geom IDs
    """
    return _vsp.FindGeomsWithName(name)

@client_wrap
def FindGeom(name, index):
    r"""
    Find and return the Geom ID with the specified name at given index. Equivalent to FindGeomsWithName( name )[index].


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD", "" )

        SetGeomName( pid, "ExamplePodName" )

        geom_id = FindGeom( "ExamplePodName", 0 )

        geom_ids = FindGeomsWithName( "ExamplePodName" )

        if  geom_ids[0] != geom_id :
            print( "---> Error: API FindGeom & FindGeomsWithName" )


    See also: FindGeomsWithName
    :param [in]: name Geom name
    :param [in]: index
    :rtype: string
    :return: Geom ID with name at specified index
    """
    return _vsp.FindGeom(name, index)

@client_wrap
def SetGeomName(geom_id, name):
    r"""
    Set the name of the specified Geom


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD", "" )

        SetGeomName( pid, "ExamplePodName" )

        geom_ids = FindGeomsWithName( "ExamplePodName" )

        if  len(geom_ids) != 1 :
            print( "---> Error: API FindGeomsWithName " )


    :param [in]: geom_id string Geom ID
    :param [in]: name Geom name
    """
    return _vsp.SetGeomName(geom_id, name)

@client_wrap
def GetGeomName(geom_id):
    r"""
    Get the name of a specific Geom


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD", "" )

        SetGeomName( pid, "ExamplePodName" )

        name_str = "Geom Name: " + GetGeomName( pid )

        print( name_str )


    :param [in]: geom_id string Geom ID
    :rtype: string
    :return: Geom name
    """
    return _vsp.GetGeomName(geom_id)

@client_wrap
def GetGeomParmIDs(geom_id):
    r"""
    Get all Parm IDs associated with this Geom Parm container


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD", "" )

        print( "---> Test Get Parm Arrays" )

        parm_array = GetGeomParmIDs( pid )

        if  len(parm_array) < 1 : print( "---> Error: API GetGeomParmIDs " )


    :param [in]: geom_id string Geom ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Parm IDs
    """
    return _vsp.GetGeomParmIDs(geom_id)

@client_wrap
def GetGeomTypeName(geom_id):
    r"""
    Get the type name of specified Geom (i.e. FUSELAGE)


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        print( "Geom Type Name: ", False )

        print( GetGeomTypeName( wing_id ) )


    :param [in]: geom_id string Geom ID
    :rtype: string
    :return: Geom type name
    """
    return _vsp.GetGeomTypeName(geom_id)

@client_wrap
def GetParm(geom_id, name, group):
    r"""
    Get Parm ID


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD" )

        lenid = GetParm( pid, "Length", "Design" )

        if  not ValidParm( lenid ) : print( "---> Error: API GetParm  " )


    :param [in]: geom_id string Geom ID
    :param [in]: name string Parm name
    :param [in]: group string Parm group name
    :rtype: string
    :return: string Parm ID
    """
    return _vsp.GetParm(geom_id, name, group)

@client_wrap
def GetGeomParent(geom_id):
    r"""
    Get the parent Geom ID for the input child Geom. "NONE" is returned if the Geom has no parent.


    .. code-block:: python

        #==== Add Parent and Child Geometry ====//
        pod1 = AddGeom( "POD" )

        pod2 = AddGeom( "POD", pod1 )

        print( "Parent ID of Pod #2: ", False )

        print( GetGeomParent( pod2 ) )


    :param [in]: geom_id string Geom ID
    :rtype: string
    :return: string Parent Geom ID
    """
    return _vsp.GetGeomParent(geom_id)

@client_wrap
def GetGeomChildren(geom_id):
    r"""
    Get the IDs for each child of the input parent Geom.


    .. code-block:: python

        #==== Add Parent and Child Geometry ====//
        pod1 = AddGeom( "POD" )

        pod2 = AddGeom( "POD", pod1 )

        pod3 = AddGeom( "POD", pod2 )

        print( "Children of Pod #1: " )

        children = GetGeomChildren( pod1 )

        for i in range(int( len(children) )):

            print( "\t", False )
            print( children[i] )


    :param [in]: geom_id string Geom ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: vector<string> Vector of child Geom IDs
    """
    return _vsp.GetGeomChildren(geom_id)

@client_wrap
def GetNumXSecSurfs(geom_id):
    r"""
    Get the number of XSecSurfs for the specified Geom


    .. code-block:: python

        #==== Add Fuselage Geometry ====//
        fuseid = AddGeom( "FUSELAGE", "" )

        num_xsec_surfs = GetNumXSecSurfs( fuseid )

        if  num_xsec_surfs != 1 : print( "---> Error: API GetNumXSecSurfs  " )


    :param [in]: geom_id string Geom ID
    :rtype: int
    :return: int Number of XSecSurfs
    """
    return _vsp.GetNumXSecSurfs(geom_id)

@client_wrap
def GetNumMainSurfs(geom_id):
    r"""
    Get the number of main surfaces for the specified Geom. Multiple main surfaces may exist for CustoGeoms, propellors, etc., but
    does not include surfaces created due to symmetry.


    .. code-block:: python

        #==== Add Prop Geometry ====//
        prop_id = AddGeom( "PROP" )

        num_surf = 0

        num_surf = GetNumMainSurfs( prop_id ) # Should be the same as the number of blades

        print( "Number of Propeller Surfaces: ", False )

        print( num_surf )


    :param [in]: geom_id string Geom ID
    :rtype: int
    :return: int Number of main surfaces
    """
    return _vsp.GetNumMainSurfs(geom_id)

@client_wrap
def GetTotalNumSurfs(geom_id):
    r"""
    Get the total number of surfaces for the specified Geom. This is equivalent to the number of main surface multiplied
    by the number of symmetric copies.


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        num_surf = 0

        num_surf = GetTotalNumSurfs( wing_id ) # Wings default with XZ symmetry on -> 2 surfaces

        print( "Total Number of Wing Surfaces: ", False )

        print( num_surf )


    :param [in]: geom_id string Geom ID
    :rtype: int
    :return: Number of main surfaces
    """
    return _vsp.GetTotalNumSurfs(geom_id)

@client_wrap
def GetGeomVSPSurfType(geom_id, main_surf_ind=0):
    r"""
    Get the VSP surface type of the specified Geom


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        if  GetGeomVSPSurfType( wing_id ) != WING_SURF :
            print( "---> Error: API GetGeomVSPSurfType " )


    See also: VSP_SURF_TYPE
    :param [in]: geom_id string Geom ID
    :param [in]: main_surf_ind Main surface index
    :rtype: int
    :return: VSP surface type enum (i.e. DISK_SURF)
    """
    return _vsp.GetGeomVSPSurfType(geom_id, main_surf_ind)

@client_wrap
def GetGeomVSPSurfCfdType(geom_id, main_surf_ind=0):
    r"""
    Get the VSP surface CFD type of the specified Geom


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        if  GetGeomVSPSurfCfdType( wing_id ) != CFD_NORMAL :
            print( "---> Error: API GetGeomVSPSurfCfdType " )


    See also: VSP_SURF_CFD_TYPE
    :param [in]: geom_id string Geom ID
    :param [in]: main_surf_ind Main surface index
    :rtype: int
    :return: VSP surface CFD type enum (i.e. CFD_TRANSPARENT)
    """
    return _vsp.GetGeomVSPSurfCfdType(geom_id, main_surf_ind)

@client_wrap
def GetGeomBBoxMax(geom_id, main_surf_ind=0, ref_frame_is_absolute=True):
    r"""
    Get the the maximum coordinate of the bounding box of a Geom with given main surface index. The Geom bounding
    box may be specified in absolute or body reference frame.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD" )

        SetParmVal( FindParm( pid, "Y_Rotation", "XForm" ), 45 )
        SetParmVal( FindParm( pid, "Z_Rotation", "XForm" ), 25 )

        Update()

        max_pnt = GetGeomBBoxMax( pid, 0, False )


    See also: GetGeomBBoxMin
    :param [in]: geom_id string Geom ID
    :param [in]: main_surf_ind Main surface index
    :param [in]: ref_frame_is_absolute Flag to specify absolute or body reference frame
    :rtype: :py:class:`vec3d`
    :return: Maximum coordinate of the bounding box
    """
    return _vsp.GetGeomBBoxMax(geom_id, main_surf_ind, ref_frame_is_absolute)

@client_wrap
def GetGeomBBoxMin(geom_id, main_surf_ind=0, ref_frame_is_absolute=True):
    r"""
    Get the the minimum coordinate of the bounding box of a Geom with given main surface index. The Geom bounding
    box may be specified in absolute or body reference frame.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD" )

        SetParmVal( FindParm( pid, "Y_Rotation", "XForm" ), 45 )
        SetParmVal( FindParm( pid, "Z_Rotation", "XForm" ), 25 )

        Update()

        min_pnt = GetGeomBBoxMin( pid, 0, False )


    See also: GetGeomBBoxMax
    :param [in]: geom_id string Geom ID
    :param [in]: main_surf_ind Main surface index
    :param [in]: ref_frame_is_absolute Flag to specify absolute or body reference frame
    :rtype: :py:class:`vec3d`
    :return: Minimum coordinate of the bounding box
    """
    return _vsp.GetGeomBBoxMin(geom_id, main_surf_ind, ref_frame_is_absolute)

@client_wrap
def AddSubSurf(geom_id, type, surfindex=0):
    r"""
    Add a sub-surface to the specified Geom


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        # Note: Parm Group for SubSurfaces in the form: "SS_" + type + "_" + count (initialized at 1)
        ss_line_id = AddSubSurf( wid, SS_LINE )                      # Add Sub Surface Line

        SetParmVal( wid, "Const_Line_Value", "SubSurface_1", 0.4 )     # Change Location


    See also: SUBSURF_TYPE
    :param [in]: geom_id string Geom ID
    :param [in]: type Sub-surface type enum (i.e. SS_RECTANGLE)
    :param [in]: surfindex Main surface index (default: 0)
    :rtype: string
    :return: Sub-surface ID
    """
    return _vsp.AddSubSurf(geom_id, type, surfindex)

@client_wrap
def GetSubSurf(*args):
    r"""
    *Overload 1:*



    Get the ID of the specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" ) # Add Wing

        ss_rec_1 = AddSubSurf( wid, SS_RECTANGLE ) # Add Sub Surface Rectangle #1

        ss_rec_2 = AddSubSurf( wid, SS_RECTANGLE ) # Add Sub Surface Rectangle #2

        print( ss_rec_2, False )

        print( " = ", False )

        print( GetSubSurf( wid, 1 ) )


    :param [in]: geom_id string Geom ID
    :param [in]: index Sub-surface index
    :rtype: string
    :return: Sub-surface ID


    |

    *Overload 2:*



    Get the ID of the specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" ) # Add Wing

        ss_rec_1 = AddSubSurf( wid, SS_RECTANGLE ) # Add Sub Surface Rectangle #1

        ss_rec_2 = AddSubSurf( wid, SS_RECTANGLE ) # Add Sub Surface Rectangle #2

        print( ss_rec_2, False )

        print( " = ", False )

        print( GetSubSurf( wid, 1 ) )


    :param [in]: geom_id string Geom ID
    :param [in]: name string Sub surface name
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: vector<string> Vector of sub-surface ID
    """
    return _vsp.GetSubSurf(*args)

@client_wrap
def DeleteSubSurf(*args):
    r"""
    *Overload 1:*



    Delete the specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_line_id = AddSubSurf( wid, SS_LINE )                      # Add Sub Surface Line
        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        print("Delete SS_Line\n")

        DeleteSubSurf( wid, ss_line_id )

        num_ss = GetNumSubSurf( wid )

        num_str = f"Number of SubSurfaces: {num_ss}\n"

        print( num_str )


    :param [in]: geom_id string Geom ID
    :param [in]: sub_id string Sub-surface ID


    |

    *Overload 2:*



    Delete the specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_line_id = AddSubSurf( wid, SS_LINE )                      # Add Sub Surface Line
        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        print("Delete SS_Line\n")

        DeleteSubSurf( ss_line_id )

        num_ss = GetNumSubSurf( wid )

        num_str = f"Number of SubSurfaces: {num_ss}\n"

        print( num_str )


    :param [in]: sub_id string Sub-surface ID
    """
    return _vsp.DeleteSubSurf(*args)

@client_wrap
def SetSubSurfName(*args):
    r"""
    *Overload 1:*



    Set the name of the specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        new_name = "New_SS_Rec_Name"

        SetSubSurfName( wid, ss_rec_id, new_name )


    :param [in]: geom_id string Geom ID
    :param [in]: sub_id string Sub-surface ID
    :param [in]: name string Sub-surface name


    |

    *Overload 2:*



    Set the name of the specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        new_name = "New_SS_Rec_Name"

        SetSubSurfName( ss_rec_id, new_name )


    :param [in]: sub_id string Sub-surface ID
    :param [in]: name string Sub-surface name
    """
    return _vsp.SetSubSurfName(*args)

@client_wrap
def GetSubSurfName(*args):
    r"""
    *Overload 1:*



    Get the name of the specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        rec_name = GetSubSurfName( wid, ss_rec_id )

        name_str = "Current Name of SS_Rectangle: " + rec_name + "\n"

        print( name_str )


    :param [in]: geom_id string Geom ID
    :param [in]: sub_id string Sub-surface ID
    :rtype: string
    :return: Sub-surface name


    |

    *Overload 2:*



    Get the name of the specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        rec_name = GetSubSurfName( wid, ss_rec_id )

        name_str = "Current Name of SS_Rectangle: " + rec_name + "\n"

        print( name_str )


    :param [in]: sub_id string Sub-surface ID
    :rtype: string
    :return: string Sub-surface name
    """
    return _vsp.GetSubSurfName(*args)

@client_wrap
def GetSubSurfIndex(sub_id):
    r"""
    Get the index of the specified sub-surface in its parent Geom's sub-surface vector


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_line_id = AddSubSurf( wid, SS_LINE )                      # Add Sub Surface Line
        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        ind = GetSubSurfIndex( ss_rec_id )

        ind_str = f"Index of SS_Rectangle: {ind}"

        print( ind_str )


    :param [in]: sub_id string Sub-surface ID
    :rtype: int
    :return: int Sub-surface index
    """
    return _vsp.GetSubSurfIndex(sub_id)

@client_wrap
def GetSubSurfIDVec(geom_id):
    r"""
    Get a vector of all sub-surface IDs for the specified geometry


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_line_id = AddSubSurf( wid, SS_LINE )                      # Add Sub Surface Line
        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        id_vec = GetSubSurfIDVec( wid )

        id_type_str = "SubSurface IDs and Type Indexes -> "

        for i in range(len(id_vec)):

            id_type_str += id_vec[i]

            id_type_str += ": "

            id_type_str += f'{GetSubSurfType(id_vec[i])}'

            id_type_str += "\t"

        id_type_str += "\n"

        print( id_type_str )


    :param [in]: geom_id string Geom ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: vector<int> Array of sub-surface IDs
    """
    return _vsp.GetSubSurfIDVec(geom_id)

@client_wrap
def GetAllSubSurfIDs():
    r"""
    Get a vector of all sub-surface IDs for the entire model
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of sub-surface IDs
    """
    return _vsp.GetAllSubSurfIDs()

@client_wrap
def GetNumSubSurf(geom_id):
    r"""
    Get the number of sub-surfaces for the specified Geom


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_line_id = AddSubSurf( wid, SS_LINE )                      # Add Sub Surface Line
        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        num_ss = GetNumSubSurf( wid )

        num_str = "Number of SubSurfaces: {num_ss}"

        print( num_str )


    :param [in]: geom_id string Geom ID
    :rtype: int
    :return: int Number of Sub-surfaces
    """
    return _vsp.GetNumSubSurf(geom_id)

@client_wrap
def GetSubSurfType(sub_id):
    r"""
    Get the type for the specified sub-surface (i.e. SS_RECTANGLE)


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_line_id = AddSubSurf( wid, SS_LINE )                      # Add Sub Surface Line
        ss_rec_id = AddSubSurf( wid, SS_RECTANGLE )                        # Add Sub Surface Rectangle

        id_vec = GetSubSurfIDVec( wid )

        id_type_str = "SubSurface IDs and Type Indexes -> "

        for i in range(len(id_vec)):

            id_type_str += id_vec[i]

            id_type_str += ": "

            id_type_str += f'{GetSubSurfType(id_vec[i])}'

            id_type_str += "\t"

        id_type_str += "\n"

        print( id_type_str )


    See also: SUBSURF_TYPE
    :param [in]: sub_id string Sub-surface ID
    :rtype: int
    :return: int Sub-surface type enum (i.e. SS_RECTANGLE)
    """
    return _vsp.GetSubSurfType(sub_id)

@client_wrap
def GetSubSurfParmIDs(sub_id):
    r"""
    Get the vector of Parm IDs for specified sub-surface


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        ss_line_id = AddSubSurf( wid, SS_LINE )                      # Add Sub Surface Line

        # Get and list all Parm info for SS_Line
        parm_id_vec = GetSubSurfParmIDs( ss_line_id )

        for i in range(len(parm_id_vec)):

            id_name_str = "\tName: " + GetParmName(parm_id_vec[i]) + ", Group: " + GetParmDisplayGroupName(parm_id_vec[i]) + ", ID: " + str(parm_id_vec[i]) + "\n"


            print( id_name_str )


    :param [in]: sub_id string Sub-surface ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: vector<string> Vector of Parm IDs
    """
    return _vsp.GetSubSurfParmIDs(sub_id)

@client_wrap
def AddFeaStruct(geom_id, init_skin=True, surfindex=0):
    r"""
    Add an FEA Structure to a specified Geom
    Warning: init_skin should ALWAYS be set to true.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: init_skin Flag to initialize the FEA Structure by creating an FEA Skin from the parent Geom's OML at surfindex
    :param [in]: surfindex Main surface index for the FEA Structure
    :rtype: int
    :return: FEA Structure index
    """
    return _vsp.AddFeaStruct(geom_id, init_skin, surfindex)

@client_wrap
def SetFeaMeshStructIndex(struct_index):
    r"""
    Sets FeaMeshMgr m_FeaMeshStructIndex member using passed in index of a FeaStructure


    .. code-block:: python


        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        SetFeaMeshStructIndex( struct_ind )

        if  len(FindGeoms()) != 0 : print( "ERROR: VSPRenew" )


    """
    return _vsp.SetFeaMeshStructIndex(struct_index)

@client_wrap
def DeleteFeaStruct(geom_id, fea_struct_ind):
    r"""
    Delete an FEA Structure and all FEA Parts and FEA SubSurfaces associated with it


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind_1 = AddFeaStruct( pod_id )

        struct_ind_2 = AddFeaStruct( pod_id )

        DeleteFeaStruct( pod_id, struct_ind_1 )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    """
    return _vsp.DeleteFeaStruct(geom_id, fea_struct_ind)

@client_wrap
def GetFeaStructID(geom_id, fea_struct_ind):
    r"""
    Get the ID of an FEA Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :rtype: string
    :return: FEA Structure ID
    """
    return _vsp.GetFeaStructID(geom_id, fea_struct_ind)

@client_wrap
def GetFeaStructIndex(struct_id):
    r"""
    Get the index of an FEA Structure in its Parent Geom's vector of Structures


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind_1 = AddFeaStruct( pod_id )

        struct_ind_2 = AddFeaStruct( pod_id )

        struct_id_2 = GetFeaStructID( pod_id, struct_ind_2 )

        DeleteFeaStruct( pod_id, struct_ind_1 )

        struct_ind_2_new = GetFeaStructIndex( struct_id_2 )


    :param [in]: struct_id FEA Structure ID
    :rtype: int
    :return: FEA Structure index
    """
    return _vsp.GetFeaStructIndex(struct_id)

@client_wrap
def GetFeaStructParentGeomID(struct_id):
    r"""
    Get the Parent Geom ID for an FEA Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )

        #==== Get Parent Geom ID and Index ====//
        parent_id = GetFeaStructParentGeomID( struct_id )


    :param [in]: struct_id FEA Structure ID
    :rtype: string
    :return: Parent Geom ID
    """
    return _vsp.GetFeaStructParentGeomID(struct_id)

@client_wrap
def GetFeaStructName(geom_id, fea_struct_ind):
    r"""
    Get the name of an FEA Structure. The FEA Structure name functions as the the Parm Container name


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Get Structure Name ====//
        parm_container_name = GetFeaStructName( pod_id, struct_ind )

        display_name = "Current Structure Parm Container Name: " + parm_container_name + "\n"

        print( display_name )


    See also: FindContainer, SetFeaStructName
    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :rtype: string
    :return: Name for the FEA Structure
    """
    return _vsp.GetFeaStructName(geom_id, fea_struct_ind)

@client_wrap
def SetFeaStructName(geom_id, fea_struct_ind, name):
    r"""
    Set the name of an FEA Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Change the Structure Name ====//
        SetFeaStructName( pod_id, struct_ind, "Example_Struct" )

        parm_container_id = FindContainer( "Example_Struct", struct_ind )

        display_id = "New Structure Parm Container ID: " + parm_container_id + "\n"

        print( display_id )


    See also: GetFeaStructName
    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :param [in]: name New name for the FEA Structure
    """
    return _vsp.SetFeaStructName(geom_id, fea_struct_ind, name)

@client_wrap
def GetFeaStructIDVec():
    r"""
    Get the IDs of all FEA Structures in the vehicle


    .. code-block:: python

        #==== Add Geometries ====//
        pod_id = AddGeom( "POD" )
        wing_id = AddGeom( "WING" )

        #==== Add FeaStructures ====//
        pod_struct_ind = AddFeaStruct( pod_id )
        wing_struct_ind = AddFeaStruct( wing_id )

        struct_id_vec = GetFeaStructIDVec()


    See also: NumFeaStructures
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of FEA Structure IDs
    """
    return _vsp.GetFeaStructIDVec()

@client_wrap
def SetFeaPartName(part_id, name):
    r"""
    Set the name of an FEA Part


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Add Bulkead ====//
        bulkhead_id = AddFeaPart( pod_id, struct_ind, FEA_SLICE )

        SetFeaPartName( bulkhead_id, "Bulkhead" )


    See also: GetFeaPartName
    :param [in]: part_id FEA Part ID
    :param [in]: name New name for the FEA Part
    """
    return _vsp.SetFeaPartName(part_id, name)

@client_wrap
def AddFeaPart(geom_id, fea_struct_ind, type):
    r"""
    Add an FEA Part to a Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Add Bulkead ====//
        bulkhead_id = AddFeaPart( pod_id, struct_ind, FEA_SLICE )

        SetParmVal( FindParm( bulkhead_id, "IncludedElements", "FeaPart" ), FEA_SHELL_AND_BEAM )

        SetParmVal( FindParm( bulkhead_id, "RelCenterLocation", "FeaPart" ), 0.15 )


    See also: FEA_PART_TYPE
    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :param [in]: type FEA Part type enum (i.e. FEA_RIB)
    :rtype: string
    :return: FEA Part ID
    """
    return _vsp.AddFeaPart(geom_id, fea_struct_ind, type)

@client_wrap
def DeleteFeaPart(geom_id, fea_struct_ind, part_id):
    r"""
    Delete an FEA Part from a Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Add Bulkead ====//
        bulkhead_id = AddFeaPart( pod_id, struct_ind, FEA_SLICE )

        #==== Add Fixed Point ====//
        fixed_id = AddFeaPart( pod_id, struct_ind, FEA_FIX_POINT )

        #==== Delete Bulkead ====//
        DeleteFeaPart( pod_id, struct_ind, bulkhead_id )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :param [in]: part_id FEA Part ID
    """
    return _vsp.DeleteFeaPart(geom_id, fea_struct_ind, part_id)

@client_wrap
def GetFeaPartID(fea_struct_id, fea_part_index):
    r"""
    Get the Parm ID of an FEA Part, identified from a FEA Structure Parm ID and FEA Part index.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )

        #==== Add Bulkead ====//
        bulkhead_id = AddFeaPart( pod_id, struct_ind, FEA_SLICE )

        Update()

        if  bulkhead_id != GetFeaPartID( struct_id, 1 ) : # These should be equivalent (index 0 is skin)

            print( "Error: GetFeaPartID" )


    :param [in]: fea_struct_id FEA Structure ID
    :param [in]: fea_part_index FEA Part index
    :rtype: string
    :return: FEA Part ID
    """
    return _vsp.GetFeaPartID(fea_struct_id, fea_part_index)

@client_wrap
def GetFeaPartName(part_id):
    r"""
    Get the name of an FEA Part


    .. code-block:: python

        #==== Add Fuselage Geometry ====//
        fuse_id = AddGeom( "FUSELAGE" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( fuse_id )

        #==== Add Bulkead ====//
        bulkhead_id = AddFeaPart( fuse_id, struct_ind, FEA_SLICE )

        name = "example_name"
        SetFeaPartName( bulkhead_id, name )

        if  name != GetFeaPartName( bulkhead_id ) : # These should be equivalent

            print( "Error: GetFeaPartName" )


    See also: SetFeaPartName
    :param [in]: part_id FEA Part ID
    :rtype: string
    :return: FEA Part name
    """
    return _vsp.GetFeaPartName(part_id)

@client_wrap
def GetFeaPartType(part_id):
    r"""
    Get the type of an FEA Part


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Add Slice ====//
        slice_id = AddFeaPart( pod_id, struct_ind, FEA_SLICE )

        if  FEA_SLICE != GetFeaPartType( slice_id ) : # These should be equivalent

            print( "Error: GetFeaPartType" )


    See also: FEA_PART_TYPE
    :param [in]: part_id FEA Part ID
    :rtype: int
    :return: FEA Part type enum
    """
    return _vsp.GetFeaPartType(part_id)

@client_wrap
def GetFeaPartIDVec(fea_struct_id):
    r"""
    Get the IDs of all FEA Parts in the given FEA Structure


    .. code-block:: python

        #==== Add Geometries ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )

        #==== Add FEA Parts ====//
        slice_id = AddFeaPart( pod_id, struct_ind, FEA_SLICE )
        dome_id = AddFeaPart( pod_id, struct_ind, FEA_DOME )

        part_id_vec = GetFeaPartIDVec( struct_id ) # Should include slice_id & dome_id


    See also: NumFeaParts
    :param [in]: fea_struct_id FEA Structure ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of FEA Part IDs
    """
    return _vsp.GetFeaPartIDVec(fea_struct_id)

@client_wrap
def GetFeaSubSurfIDVec(fea_struct_id):
    r"""
    Get the IDs of all FEA SubSurfaces in the given FEA Structure


    .. code-block:: python

        #==== Add Geometries ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )

        #==== Add SubSurfaces ====//
        line_array_id = AddFeaSubSurf( pod_id, struct_ind, SS_LINE_ARRAY )
        rectangle_id = AddFeaSubSurf( pod_id, struct_ind, SS_RECTANGLE )

        part_id_vec = GetFeaSubSurfIDVec( struct_id ) # Should include line_array_id & rectangle_id


    See also: NumFeaSubSurfs
    :param [in]: fea_struct_id FEA Structure ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of FEA Part IDs
    """
    return _vsp.GetFeaSubSurfIDVec(fea_struct_id)

@client_wrap
def SetFeaPartPerpendicularSparID(part_id, perpendicular_spar_id):
    r"""
    Set the ID of the perpendicular spar for an FEA Rib or Rib Array. Note, the FEA Rib or Rib Array should have "SPAR_NORMAL"
    set for the "PerpendicularEdgeType" Parm. If it is not, the ID will still be set, but the orientation of the Rib or Rib
    Array will not change.


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        #==== Add FeaStructure to Wing ====//
        struct_ind = AddFeaStruct( wing_id )

        #==== Add Rib ====//
        rib_id = AddFeaPart( wing_id, struct_ind, FEA_RIB )

        #==== Add Spars ====//
        spar_id_1 = AddFeaPart( wing_id, struct_ind, FEA_SPAR )
        spar_id_2 = AddFeaPart( wing_id, struct_ind, FEA_SPAR )

        SetParmVal( FindParm( spar_id_1, "RelCenterLocation", "FeaPart" ), 0.25 )
        SetParmVal( FindParm( spar_id_2, "RelCenterLocation", "FeaPart" ), 0.75 )

        #==== Set Perpendicular Edge type to SPAR ====//
        SetParmVal( FindParm( rib_id, "PerpendicularEdgeType", "FeaRib" ), SPAR_NORMAL )

        SetFeaPartPerpendicularSparID( rib_id, spar_id_2 )

        if  spar_id_2 != GetFeaPartPerpendicularSparID( rib_id ) :
            print( "Error: SetFeaPartPerpendicularSparID" )


    See also: FEA_RIB_NORMAL, GetFeaPartPerpendicularSparID
    :param [in]: part_id FEA Part ID (Rib or Rib Array Type)
    :param [in]: perpendicular_spar_id FEA Spar ID
    """
    return _vsp.SetFeaPartPerpendicularSparID(part_id, perpendicular_spar_id)

@client_wrap
def GetFeaPartPerpendicularSparID(part_id):
    r"""
    Get the ID of the perpendicular spar for an FEA Rib or Rib Array. Note, the FEA Rib or Rib Array doesn't have to have "SPAR_NORMAL"
    set for the "PerpendicularEdgeType" Parm for this function to still return a value.


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        #==== Add FeaStructure to Wing ====//
        struct_ind = AddFeaStruct( wing_id )

        #==== Add Rib ====//
        rib_id = AddFeaPart( wing_id, struct_ind, FEA_RIB )

        #==== Add Spars ====//
        spar_id_1 = AddFeaPart( wing_id, struct_ind, FEA_SPAR )
        spar_id_2 = AddFeaPart( wing_id, struct_ind, FEA_SPAR )

        SetParmVal( FindParm( spar_id_1, "RelCenterLocation", "FeaPart" ), 0.25 )
        SetParmVal( FindParm( spar_id_2, "RelCenterLocation", "FeaPart" ), 0.75 )

        #==== Set Perpendicular Edge type to SPAR ====//
        SetParmVal( FindParm( rib_id, "PerpendicularEdgeType", "FeaRib" ), SPAR_NORMAL )

        SetFeaPartPerpendicularSparID( rib_id, spar_id_2 )

        if  spar_id_2 != GetFeaPartPerpendicularSparID( rib_id ) :
            print( "Error: GetFeaPartPerpendicularSparID" )


    See also: FEA_RIB_NORMAL, SetFeaPartPerpendicularSparID
    :param [in]: part_id FEA Part ID (Rib or Rib Array Type)
    :rtype: string
    :return: Perpendicular FEA Spar ID
    """
    return _vsp.GetFeaPartPerpendicularSparID(part_id)

@client_wrap
def AddFeaSubSurf(geom_id, fea_struct_ind, type):
    r"""
    Add an FEA SubSurface to a Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Add LineArray ====//
        line_array_id = AddFeaSubSurf( pod_id, struct_ind, SS_LINE_ARRAY )

        SetParmVal( FindParm( line_array_id, "ConstLineType", "SS_LineArray" ), 1 ) # Constant W

        SetParmVal( FindParm( line_array_id, "Spacing", "SS_LineArray" ), 0.25 )


    See also: SUBSURF_TYPE
    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :param [in]: type FEA SubSurface type enum (i.e. SS_ELLIPSE)
    :rtype: string
    :return: FEA SubSurface ID
    """
    return _vsp.AddFeaSubSurf(geom_id, fea_struct_ind, type)

@client_wrap
def DeleteFeaSubSurf(geom_id, fea_struct_ind, ss_id):
    r"""
    Delete an FEA SubSurface from a Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Add LineArray ====//
        line_array_id = AddFeaSubSurf( pod_id, struct_ind, SS_LINE_ARRAY )

        #==== Add Rectangle ====//
        rect_id = AddFeaSubSurf( pod_id, struct_ind, SS_RECTANGLE )

        #==== Delete LineArray ====//
        DeleteFeaSubSurf( pod_id, struct_ind, line_array_id )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :param [in]: ss_id FEA SubSurface ID
    """
    return _vsp.DeleteFeaSubSurf(geom_id, fea_struct_ind, ss_id)

@client_wrap
def GetFeaSubSurfIndex(ss_id):
    r"""
    Get the index of an FEA SubSurface give the SubSurface ID


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Add Slice ====//
        slice_id = AddFeaPart( pod_id, struct_ind, FEA_SLICE )

        #==== Add LineArray ====//
        line_array_id = AddFeaSubSurf( pod_id, struct_ind, SS_LINE_ARRAY )

        #==== Add Rectangle ====//
        rect_id = AddFeaSubSurf( pod_id, struct_ind, SS_RECTANGLE )

        if  1 != GetFeaSubSurfIndex( rect_id ) : # These should be equivalent

            print( "Error: GetFeaSubSurfIndex" )


    :param [in]: ss_id FEA SubSurface ID
    :rtype: int
    :return: FEA SubSurface Index
    """
    return _vsp.GetFeaSubSurfIndex(ss_id)

@client_wrap
def NumFeaStructures():
    r"""
    Get the total number of FEA Subsurfaces in the vehicle


    .. code-block:: python

        #==== Add Pod Geometry ====//
        wing_id = AddGeom( "WING" )

        #==== Add FeaStructure to Pod ====//
        struct_1 = AddFeaStruct( wing_id )
        struct_2 = AddFeaStruct( wing_id )

        if  NumFeaStructures() != 2 :
            print( "Error: NumFeaStructures" )


    See also: GetFeaStructIDVec
    :rtype: int
    :return: Total Number of FEA Structures
    """
    return _vsp.NumFeaStructures()

@client_wrap
def NumFeaParts(fea_struct_id):
    r"""
    Get the number of FEA Parts for a particular FEA Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )

        #==== Add FEA Parts ====//
        slice_id = AddFeaPart( pod_id, struct_ind, FEA_SLICE )
        dome_id = AddFeaPart( pod_id, struct_ind, FEA_DOME )

        if  NumFeaParts( struct_id ) != 3 : # Includes FeaSkin

            print( "Error: NumFeaParts" )


    See also: GetFeaPartIDVec
    :param [in]: fea_struct_id FEA Structure ID
    :rtype: int
    :return: Number of FEA Parts
    """
    return _vsp.NumFeaParts(fea_struct_id)

@client_wrap
def NumFeaSubSurfs(fea_struct_id):
    r"""
    Get the number of FEA Subsurfaces for a particular FEA Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        wing_id = AddGeom( "WING" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( wing_id )

        struct_id = GetFeaStructID( wing_id, struct_ind )

        #==== Add SubSurfaces ====//
        line_array_id = AddFeaSubSurf( wing_id, struct_ind, SS_LINE_ARRAY )
        rectangle_id = AddFeaSubSurf( wing_id, struct_ind, SS_RECTANGLE )

        if  NumFeaSubSurfs( struct_id ) != 2 :
            print( "Error: NumFeaSubSurfs" )


    See also: GetFeaSubSurfIDVec
    :param [in]: fea_struct_id FEA Structure ID
    :rtype: int
    :return: Number of FEA SubSurfaces
    """
    return _vsp.NumFeaSubSurfs(fea_struct_id)

@client_wrap
def AddFeaMaterial():
    r"""
    Add an FEA Material the FEA Mesh material library. Materials are available across all Geoms and Structures.


    .. code-block:: python

        #==== Create FeaMaterial ====//
        mat_id = AddFeaMaterial()

        SetParmVal( FindParm( mat_id, "MassDensity", "FeaMaterial" ), 0.016 )


    :rtype: string
    :return: FEA Material ID
    """
    return _vsp.AddFeaMaterial()

@client_wrap
def AddFeaProperty(property_type=0):
    r"""
    Add aa FEA Property the FEA Mesh property library. Properties are available across all Geoms and Structures. Currently only beam and
    shell properties are available. Note FEA_SHELL_AND_BEAM is not a valid property type.


    .. code-block:: python

        #==== Create FeaProperty ====//
        prop_id = AddFeaProperty()

        SetParmVal( FindParm( prop_id, "Thickness", "FeaProperty" ), 0.01 )


    See also: FEA_PART_ELEMENT_TYPE
    :param [in]: property_type FEA Property type enum (i.e. FEA_SHELL).
    :rtype: string
    :return: FEA Property ID
    """
    return _vsp.AddFeaProperty(property_type)

@client_wrap
def SetFeaMeshVal(geom_id, fea_struct_ind, type, val):
    r"""
    Set the value of a particular FEA Mesh option for the specified Structure. Note, FEA Mesh makes use of enums initially created for CFD Mesh
    but not all CFD Mesh options are available for FEA Mesh.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Adjust FeaMeshSettings ====//
        SetFeaMeshVal( pod_id, struct_ind, CFD_MAX_EDGE_LEN, 0.75 )

        SetFeaMeshVal( pod_id, struct_ind, CFD_MIN_EDGE_LEN, 0.2 )


    See also: CFD_CONTROL_TYPE
    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :param [in]: type FEA Mesh option type enum (i.e. CFD_MAX_EDGE_LEN)
    :param [in]: val Value the option is set to
    """
    return _vsp.SetFeaMeshVal(geom_id, fea_struct_ind, type, val)

@client_wrap
def SetFeaMeshFileName(geom_id, fea_struct_ind, file_type, file_name):
    r"""
    Set the name of a particular FEA Mesh output file for a specified Structure


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )

        #=== Set Export File Name ===//
        export_name = "FEAMeshTest_calculix.dat"

        #==== Get Parent Geom ID and Index ====//
        parent_id = GetFeaStructParentGeomID( struct_id ) # same as pod_id

        SetFeaMeshFileName( parent_id, struct_ind, FEA_CALCULIX_FILE_NAME, export_name )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind FEA Structure index
    :param [in]: file_type FEA output file type enum (i.e. FEA_EXPORT_TYPE)
    :param [in]: file_name Name for the output file
    """
    return _vsp.SetFeaMeshFileName(geom_id, fea_struct_ind, file_type, file_name)

@client_wrap
def ComputeFeaMesh(*args):
    r"""
    *Overload 1:*



    Compute an FEA Mesh for a Structure. Only a single output file can be generated with this function.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )

        #==== Generate FEA Mesh and Export ====//
        print( "--> Generating FeaMesh " )

        #==== Get Parent Geom ID and Index ====//
        parent_id = GetFeaStructParentGeomID( struct_id ) # same as pod_id

        ComputeFeaMesh( parent_id, struct_ind, FEA_CALCULIX_FILE_NAME )


    See also: SetFeaMeshFileName, FEA_EXPORT_TYPE
    :param [in]: geom_id string Parent Geom ID
    :param [in]: fea_struct_ind int FEA Structure index
    :param [in]: file_type int FEA output file type enum (i.e. FEA_EXPORT_TYPE)


    |

    *Overload 2:*



    Compute an FEA Mesh for a Structure. Only a single output file can be generated with this function.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        struct_id = GetFeaStructID( pod_id, struct_ind )

        #==== Generate FEA Mesh and Export ====//
        print( string( "--> Generating FeaMesh " ) )

        #==== Get Parent Geom ID and Index ====//
        parent_id = GetFeaStructParentGeomID( struct_id ) # same as pod_id

        Could also call ComputeFeaMesh ( struct_id, FEA_CALCULIX_FILE_NAME )


    See also: SetFeaMeshFileName, FEA_EXPORT_TYPE
    :param [in]: struct_id string FEA Structure index
    :param [in]: file_type int FEA output file type enum (i.e. FEA_EXPORT_TYPE)
    """
    return _vsp.ComputeFeaMesh(*args)

@client_wrap
def CutXSec(geom_id, index):
    r"""
    Cut a cross-section from the specified geometry and maintain it in memory


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        #==== Insert, Cut, Paste Example ====//
        InsertXSec( fid, 1, XS_ROUNDED_RECTANGLE )         # Insert A Cross-Section

        CopyXSec( fid, 2 )                                 # Copy Just Created XSec To Clipboard

        PasteXSec( fid, 1 )                                # Paste Clipboard

        CutXSec( fid, 2 )                                  # Cut Created XSec


    See also: PasteXSec
    :param [in]: geom_id string Geom ID
    :param [in]: index XSec index
    """
    return _vsp.CutXSec(geom_id, index)

@client_wrap
def CopyXSec(geom_id, index):
    r"""
    Copy a cross-section from the specified geometry and maintain it in memory


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Copy XSec To Clipboard
        CopyXSec( sid, 1 )

        # Paste To XSec 3
        PasteXSec( sid, 3 )


    See also: PasteXSec
    :param [in]: geom_id string Geom ID
    :param [in]: index XSec index
    """
    return _vsp.CopyXSec(geom_id, index)

@client_wrap
def PasteXSec(geom_id, index):
    r"""
    Paste the cross-section currently held in memory to the specified geometry


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Copy XSec To Clipboard
        CopyXSec( sid, 1 )

        # Paste To XSec 3
        PasteXSec( sid, 3 )


    See also: CutXSec, CopyXSec
    :param [in]: geom_id string Geom ID
    :param [in]: index XSec index
    """
    return _vsp.PasteXSec(geom_id, index)

@client_wrap
def InsertXSec(geom_id, index, type):
    r"""
    Insert a cross-section of particular type to the specified geometry after the given index


    .. code-block:: python

        wing_id = AddGeom( "WING" )

        #===== Add XSec ====//
        InsertXSec( wing_id, 1, XS_SIX_SERIES )


    See also: XSEC_CRV_TYPE
    :param [in]: geom_id string Geom ID
    :param [in]: index XSec index
    :param [in]: type XSec type enum (i.e. XS_GENERAL_FUSE)
    """
    return _vsp.InsertXSec(geom_id, index, type)

@client_wrap
def SetDriverGroup(geom_id, section_index, driver_0, driver_1=-1, driver_2=-1):
    r"""
    Set the driver group for a wing section or a XSecCurve. Care has to be taken when setting these driver groups to ensure a valid combination.


    .. code-block:: python

        #==== Add Wing Geometry and Set Parms ====//
        wing_id = AddGeom( "WING", "" )

        #==== Set Wing Section Controls ====//
        SetDriverGroup( wing_id, 1, AR_WSECT_DRIVER, ROOTC_WSECT_DRIVER, TIPC_WSECT_DRIVER )

        Update()

        #==== Set Parms ====//
        SetParmVal( wing_id, "Root_Chord", "XSec_1", 2 )
        SetParmVal( wing_id, "Tip_Chord", "XSec_1", 1 )

        Update()


    See also: WING_DRIVERS, XSEC_DRIVERS
    :param [in]: geom_id string Geom ID
    :param [in]: section_index Wing section index
    :param [in]: driver_0 First driver enum (i.e. SPAN_WSECT_DRIVER)
    :param [in]: driver_1 Second driver enum (i.e. ROOTC_WSECT_DRIVER)
    :param [in]: driver_2 Third driver enum (i.e. TIPC_WSECT_DRIVER)
    """
    return _vsp.SetDriverGroup(geom_id, section_index, driver_0, driver_1, driver_2)

@client_wrap
def GetXSecSurf(geom_id, index):
    r"""
    Get the XSecSurf ID for a particular Geom and XSecSurf index


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )


    :param [in]: geom_id string Geom ID
    :param [in]: index XSecSurf index
    :rtype: string
    :return: XSecSurf ID
    """
    return _vsp.GetXSecSurf(geom_id, index)

@client_wrap
def GetNumXSec(xsec_surf_id):
    r"""
    Get number of XSecs in an XSecSurf


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        # Flatten ends
        num_xsecs = GetNumXSec( xsec_surf )

        for i in range(num_xsecs):

            xsec = GetXSec( xsec_surf, i )

            SetXSecTanAngles( xsec, XSEC_BOTH_SIDES, 0, -1.0e12, -1.0e12, -1.0e12 )       # Set Tangent Angles At Cross Section

            SetXSecTanStrengths( xsec, XSEC_BOTH_SIDES, 0.0, -1.0e12, -1.0e12, -1.0e12 )  # Set Tangent Strengths At Cross Section


    :param [in]: xsec_surf_id XSecSurf ID
    :rtype: int
    :return: Number of XSecs
    """
    return _vsp.GetNumXSec(xsec_surf_id)

@client_wrap
def GetXSec(xsec_surf_id, xsec_index):
    r"""
    Get Xsec ID for a particular XSecSurf at given index


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        # Identify XSec 1
        xsec_1 = GetXSec( xsec_surf, 1 )


    :param [in]: xsec_surf_id XSecSurf ID
    :param [in]: xsec_index Xsec index
    :rtype: string
    :return: Xsec ID
    """
    return _vsp.GetXSec(xsec_surf_id, xsec_index)

@client_wrap
def ChangeXSecShape(xsec_surf_id, xsec_index, type):
    r"""
    Change the shape of a particular XSec, identified by an XSecSurf ID and XSec index


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        # Set XSec 1 & 2 to Edit Curve type
        ChangeXSecShape( xsec_surf, 1, XS_EDIT_CURVE )
        ChangeXSecShape( xsec_surf, 2, XS_EDIT_CURVE )

        xsec_2 = GetXSec( xsec_surf, 2 )

        if  GetXSecShape( xsec_2 ) != XS_EDIT_CURVE :
            print( "Error: ChangeXSecShape" )


    See also: XSEC_CRV_TYPE
    :param [in]: xsec_surf_id XSecSurf ID
    :param [in]: xsec_index Xsec index
    :param [in]: type Xsec type enum (i.e. XS_ELLIPSE)
    """
    return _vsp.ChangeXSecShape(xsec_surf_id, xsec_index, type)

@client_wrap
def SetXSecSurfGlobalXForm(xsec_surf_id, mat):
    r"""
    Set the global surface transform matrix for given XSecSurf
    :param [in]: xsec_surf_id XSecSurf ID
    :param [in]: mat Transformation matrix
    """
    return _vsp.SetXSecSurfGlobalXForm(xsec_surf_id, mat)

@client_wrap
def GetXSecSurfGlobalXForm(xsec_surf_id):
    r"""
    Get the global surface transform matrix for given XSecSurf
    :param [in]: xsec_surf_id XSecSurf ID
    :rtype: :py:class:`Matrix4d`
    :return: Transformation matrix
    """
    return _vsp.GetXSecSurfGlobalXForm(xsec_surf_id)

@client_wrap
def GetXSecShape(xsec_id):
    r"""
    Get the shape of an XSec


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_EDIT_CURVE )

        xsec = GetXSec( xsec_surf, 1 )

        if  GetXSecShape( xsec ) != XS_EDIT_CURVE : print( "ERROR: GetXSecShape" )


    See also: XSEC_CRV_TYPE
    :param [in]: xsec_id XSec ID
    :rtype: int
    :return: XSec type enum (i.e. XS_ELLIPSE)
    """
    return _vsp.GetXSecShape(xsec_id)

@client_wrap
def GetXSecWidth(xsec_id):
    r"""
    Get the width of an XSec. Note that POINT type XSecs have a width and height of 0, regardless of what width and height it is set to.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 2 ) # Get 2nd to last XSec

        SetXSecWidthHeight( xsec, 3.0, 6.0 )

        if  abs( GetXSecWidth( xsec ) - 3.0 ) > 1e-6 : print( "---> Error: API Get/Set Width " )


    See also: SetXSecWidth
    :param [in]: xsec_id XSec ID
    :rtype: float
    :return: Xsec width
    """
    return _vsp.GetXSecWidth(xsec_id)

@client_wrap
def GetXSecHeight(xsec_id):
    r"""
    Get the height of an XSec. Note that POINT type XSecs have a width and height of 0, regardless of what width and height it is set to.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 2 ) # Get 2nd to last XSec

        SetXSecWidthHeight( xsec, 3.0, 6.0 )

        if  abs( GetXSecHeight( xsec ) - 6.0 ) > 1e-6 : print( "---> Error: API Get/Set Width " )


    See also: SetXSecHeight
    :param [in]: xsec_id XSec ID
    :rtype: float
    :return: Xsec height
    """
    return _vsp.GetXSecHeight(xsec_id)

@client_wrap
def SetXSecWidthHeight(xsec_id, w, h):
    r"""
    Set the width and height of an XSec. Note, if the XSec is an EDIT_CURVE type and PreserveARFlag is true, the input width value will be
    ignored and instead set from on the input height and aspect ratio. Use SetXSecWidth and SetXSecHeight directly to avoid this.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        # Identify XSec 2
        xsec_2 = GetXSec( xsec_surf, 2 )

        SetXSecWidthHeight( xsec_2, 1.5, 1.5 )


    See also: SetXSecWidth, SetXSecHeight
    :param [in]: xsec_id XSec ID
    :param [in]: w Xsec width
    :param [in]: h Xsec height
    """
    return _vsp.SetXSecWidthHeight(xsec_id, w, h)

@client_wrap
def SetXSecWidth(xsec_id, w):
    r"""
    Set the width of an XSec. Note that POINT type XSecs have a width and height of 0, regardless of what is input to SetXSecWidth.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        # Identify XSec 2
        xsec_2 = GetXSec( xsec_surf, 2 )

        SetXSecWidth( xsec_2, 1.5 )


    See also: GetXSecWidth
    :param [in]: xsec_id XSec ID
    :param [in]: w Xsec width
    """
    return _vsp.SetXSecWidth(xsec_id, w)

@client_wrap
def SetXSecHeight(xsec_id, h):
    r"""
    Set the height of an XSec. Note that POINT type XSecs have a width and height of 0, regardless of what is input to SetXSecHeight.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        # Identify XSec 2
        xsec_2 = GetXSec( xsec_surf, 2 )

        SetXSecHeight( xsec_2, 1.5 )


    See also: GetXSecHeight
    :param [in]: xsec_id XSec ID
    :param [in]: h Xsec height
    """
    return _vsp.SetXSecHeight(xsec_id, h)

@client_wrap
def GetXSecParmIDs(xsec_id):
    r"""
    Get all Parm IDs for specified XSec Parm Container


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        parm_array = GetXSecParmIDs( xsec )

        if  len(parm_array) < 1 : print( "---> Error: API GetXSecParmIDs " )


    :param [in]: xsec_id XSec ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Parm IDs
    """
    return _vsp.GetXSecParmIDs(xsec_id)

@client_wrap
def GetXSecParm(xsec_id, name):
    r"""
    Get a specific Parm ID from an Xsec


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        if  not ValidParm( wid ) : print( "---> Error: API GetXSecParm " )


    :param [in]: xsec_id XSec ID
    :param [in]: name Parm name
    :rtype: string
    :return: Parm ID
    """
    return _vsp.GetXSecParm(xsec_id, name)

@client_wrap
def ReadFileXSec(xsec_id, file_name):
    r"""
    Read in XSec shape from fuselage (*.fsx) file and set to the specified XSec. The XSec must be of type XS_FILE_FUSE.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, 2, XS_FILE_FUSE )

        xsec = GetXSec( xsec_surf, 2 )

        vec_array = ReadFileXSec(xsec, "TestXSec.fxs")



    :param [in]: xsec_id XSec ID
    :param [in]: file_name Fuselage XSec file name
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: Array of coordinate points read from the file and set to the XSec
    """
    return _vsp.ReadFileXSec(xsec_id, file_name)

@client_wrap
def SetXSecPnts(xsec_id, pnt_vec):
    r"""
    Set the coordinate points for a specific XSec. The XSec must be of type XS_FILE_FUSE.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, 2, XS_FILE_FUSE )

        xsec = GetXSec( xsec_surf, 2 )

        vec_array = ReadFileXSec(xsec, "TestXSec.fxs")


        if  len(vec_array) > 0 :
            vec_array[1] = vec_array[1] * 2.0
            vec_array[3] = vec_array[3] * 2.0

            SetXSecPnts( xsec, vec_array )


    :param [in]: xsec_id string XSec ID
    :param [in]: pnt_vec vector<vec3d> Vector of XSec coordinate points
    """
    return _vsp.SetXSecPnts(xsec_id, pnt_vec)

@client_wrap
def ComputeXSecPnt(xsec_id, fract):
    r"""
    Compute 3D coordinate for a point on an XSec curve given the parameter value (U) along the curve


    .. code-block:: python

        #==== Add Geom ====//
        stack_id = AddGeom( "STACK" )

        #==== Get The XSec Surf ====//
        xsec_surf = GetXSecSurf( stack_id, 0 )

        xsec = GetXSec( xsec_surf, 2 )

        u_fract = 0.25

        pnt = ComputeXSecPnt(xsec, u_fract)



    :param [in]: xsec_id string XSec ID
    :param [in]: fract double Curve parameter value (range: 0 - 1)
    :rtype: :py:class:`vec3d`
    :return: vec3d 3D coordinate point
    """
    return _vsp.ComputeXSecPnt(xsec_id, fract)

@client_wrap
def ComputeXSecTan(xsec_id, fract):
    r"""
    Compute the tangent vector of a point on an XSec curve given the parameter value (U) along the curve


    .. code-block:: python

        #==== Add Geom ====//
        stack_id = AddGeom( "STACK" )

        #==== Get The XSec Surf ====//
        xsec_surf = GetXSecSurf( stack_id, 0 )

        xsec = GetXSec( xsec_surf, 2 )

        u_fract = 0.25

        tan = ComputeXSecTan( xsec, u_fract )


    :param [in]: xsec_id string XSec ID
    :param [in]: fract double Curve parameter value (range: 0 - 1)
    :rtype: :py:class:`vec3d`
    :return: vec3d Tangent vector
    """
    return _vsp.ComputeXSecTan(xsec_id, fract)

@client_wrap
def ResetXSecSkinParms(xsec_id):
    r"""
    Reset all skinning Parms for a specified XSec. Set top, bottom, left, and right strengths, slew, angle, and curvature to 0. Set all symmetry and equality conditions to false.


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        xsec_surf = GetXSecSurf( fid, 0 )           # Get First (and Only) XSec Surf

        num_xsecs = GetNumXSec( xsec_surf )

        xsec = GetXSec( xsec_surf, 1 )

        SetXSecTanAngles( xsec, XSEC_BOTH_SIDES, 0.0, -1.0e12, -1.0e12, -1.0e12 )       # Set Tangent Angles At Cross Section
        SetXSecContinuity( xsec, 1 )                       # Set Continuity At Cross Section

        ResetXSecSkinParms( xsec )


    :param [in]: xsec_id string XSec ID
    """
    return _vsp.ResetXSecSkinParms(xsec_id)

@client_wrap
def SetXSecContinuity(xsec_id, cx):
    r"""
    Set C-type continuity enforcement for a particular XSec


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        xsec_surf = GetXSecSurf( fid, 0 )           # Get First (and Only) XSec Surf

        num_xsecs = GetNumXSec( xsec_surf )

        for i in range(num_xsecs):

            xsec = GetXSec( xsec_surf, i )

            SetXSecContinuity( xsec, 1 )                       # Set Continuity At Cross Section


    :param [in]: xsec_id string XSec ID
    :param [in]: cx int Continuity level (0, 1, or 2)
    """
    return _vsp.SetXSecContinuity(xsec_id, cx)

@client_wrap
def SetXSecTanAngles(xsec_id, side, top, right, bottom, left):
    r"""
    Set the tangent angles for the specified XSec


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        num_xsecs = GetNumXSec( xsec_surf )

        for i in range(num_xsecs):

            xsec = GetXSec( xsec_surf, i )

            SetXSecTanAngles( xsec, XSEC_BOTH_SIDES, 10.0, -1.0e12, -1.0e12, -1.0e12 )       # Set Tangent Angles At Cross Section


    See also: XSEC_SIDES_TYPE
    :param [in]: xsec_id string XSec ID
    :param [in]: side int Side type enum (i.e. XSEC_BOTH_SIDES)
    :param [in]: top double Top angle (degrees)
    :param [in]: right double Right angle (degrees)
    :param [in]: bottom double Bottom angle (degrees)
    :param [in]: left double Left angle (degrees)
    """
    return _vsp.SetXSecTanAngles(xsec_id, side, top, right, bottom, left)

@client_wrap
def SetXSecTanSlews(xsec_id, side, top, right, bottom, left):
    r"""
    Set the tangent slew angles for the specified XSec


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        num_xsecs = GetNumXSec( xsec_surf )

        for i in range(num_xsecs):

            xsec = GetXSec( xsec_surf, i )

            SetXSecTanSlews( xsec, XSEC_BOTH_SIDES, 5.0, -1.0e12, -1.0e12, -1.0e12 )       # Set Tangent Slews At Cross Section


    See also: XSEC_SIDES_TYPE
    :param [in]: xsec_id XSec ID
    :param [in]: side Side type enum (i.e. XSEC_BOTH_SIDES)
    :param [in]: top Top angle (degrees)
    :param [in]: right Right angle (degrees)
    :param [in]: bottom Bottom angle (degrees)
    :param [in]: left Left angle (degrees)
    """
    return _vsp.SetXSecTanSlews(xsec_id, side, top, right, bottom, left)

@client_wrap
def SetXSecTanStrengths(xsec_id, side, top, right, bottom, left):
    r"""
    Set the tangent strengths for the specified XSec


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        # Flatten ends
        num_xsecs = GetNumXSec( xsec_surf )

        for i in range(num_xsecs):

            xsec = GetXSec( xsec_surf, i )

            SetXSecTanStrengths( xsec, XSEC_BOTH_SIDES, 0.8, -1.0e12, -1.0e12, -1.0e12 )  # Set Tangent Strengths At Cross Section


    See also: XSEC_SIDES_TYPE
    :param [in]: xsec_id XSec ID
    :param [in]: side Side type enum (i.e. XSEC_BOTH_SIDES)
    :param [in]: top Top strength
    :param [in]: right Right strength
    :param [in]: bottom Bottom strength
    :param [in]: left Left strength
    """
    return _vsp.SetXSecTanStrengths(xsec_id, side, top, right, bottom, left)

@client_wrap
def SetXSecCurvatures(xsec_id, side, top, right, bottom, left):
    r"""
    Set curvatures for the specified XSec


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        # Flatten ends
        num_xsecs = GetNumXSec( xsec_surf )

        for i in range(num_xsecs):

            xsec = GetXSec( xsec_surf, i )

            SetXSecCurvatures( xsec, XSEC_BOTH_SIDES, 0.2, -1.0e12, -1.0e12, -1.0e12 )  # Set Tangent Strengths At Cross Section


    See also: XSEC_SIDES_TYPE
    :param [in]: xsec_id XSec ID
    :param [in]: side Side type enum (i.e. XSEC_BOTH_SIDES)
    :param [in]: top Top curvature
    :param [in]: right Right curvature
    :param [in]: bottom Bottom curvature
    :param [in]: left Left curvature
    """
    return _vsp.SetXSecCurvatures(xsec_id, side, top, right, bottom, left)

@client_wrap
def ReadFileAirfoil(xsec_id, file_name):
    r"""
    Read in XSec shape from airfoil file and set to the specified XSec. The XSec must be of type XS_FILE_AIRFOIL. Airfoil files may be in Lednicer or Selig format with *.af or *.dat extensions.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_FILE_AIRFOIL )

        xsec = GetXSec( xsec_surf, 1 )

        ReadFileAirfoil( xsec, "airfoil/N0012_VSP.af" )


    :param [in]: xsec_id XSec ID
    :param [in]: file_name Airfoil XSec file name
    """
    return _vsp.ReadFileAirfoil(xsec_id, file_name)

@client_wrap
def SetAirfoilUpperPnts(xsec_id, up_pnt_vec):
    r"""
    Set the upper points for an airfoil. The XSec must be of type XS_FILE_AIRFOIL.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_FILE_AIRFOIL )

        xsec = GetXSec( xsec_surf, 1 )

        ReadFileAirfoil( xsec, "airfoil/N0012_VSP.af" )

        up_array = GetAirfoilUpperPnts( xsec )

        for i in range(int( len(up_array) )):

            up_array[i].scale_y( 2.0 )

        SetAirfoilUpperPnts( xsec, up_array )


    :param [in]: xsec_id XSec ID
    :param [in]: up_pnt_vec Array of points defining the upper surface of the airfoil
    """
    return _vsp.SetAirfoilUpperPnts(xsec_id, up_pnt_vec)

@client_wrap
def SetAirfoilLowerPnts(xsec_id, low_pnt_vec):
    r"""
    Set the lower points for an airfoil. The XSec must be of type XS_FILE_AIRFOIL.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_FILE_AIRFOIL )

        xsec = GetXSec( xsec_surf, 1 )

        ReadFileAirfoil( xsec, "airfoil/N0012_VSP.af" )

        low_array = GetAirfoilLowerPnts( xsec )

        for i in range(int( len(low_array) )):

            low_array[i].scale_y( 0.5 )

        SetAirfoilUpperPnts( xsec, low_array )


    :param [in]: xsec_id XSec ID
    :param [in]: low_pnt_vec Array of points defining the lower surface of the airfoil
    """
    return _vsp.SetAirfoilLowerPnts(xsec_id, low_pnt_vec)

@client_wrap
def SetAirfoilPnts(xsec_id, up_pnt_vec, low_pnt_vec):
    r"""
    Set the upper and lower points for an airfoil. The XSec must be of type XS_FILE_AIRFOIL.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_FILE_AIRFOIL )

        xsec = GetXSec( xsec_surf, 1 )

        ReadFileAirfoil( xsec, "airfoil/N0012_VSP.af" )

        up_array = GetAirfoilUpperPnts( xsec )

        low_array = GetAirfoilLowerPnts( xsec )

        for i in range(int( len(up_array) )):

            up_array[i].scale_y( 2.0 )

            low_array[i].scale_y( 0.5 )

        SetAirfoilPnts( xsec, up_array, low_array )


    :param [in]: xsec_id XSec ID
    :param [in]: up_pnt_vec Array of points defining the upper surface of the airfoil
    :param [in]: low_pnt_vec Array of points defining the lower surface of the airfoil
    """
    return _vsp.SetAirfoilPnts(xsec_id, up_pnt_vec, low_pnt_vec)

@client_wrap
def GetHersheyBarLiftDist(npts, alpha, Vinf, span, full_span_flag=False):
    r"""
    Get the theoretical lift (Cl) distribution for a Hershey Bar wing with unit chord length using Glauert's Method. This function was initially created to compare VSPAERO results to Lifting Line Theory.
    If full_span_flag is set to true symmetry is applied to the results.


    .. code-block:: python

        pi = 3.14159265358979323846
        # Compute theoretical lift and drag distributions using 100 points
        Vinf = 100

        halfAR = 20

        alpha_deg = 10

        n_pts = 100

        cl_dist_theo = GetHersheyBarLiftDist( int( n_pts ), alpha_deg*pi/180, Vinf, ( 2 * halfAR ), False )

        cd_dist_theo = GetHersheyBarDragDist( int( n_pts ), alpha_deg*pi/180, Vinf, ( 2 * halfAR ), False )


    :param [in]: npts Number of points along the span to assess
    :param [in]: alpha Wing angle of attack (Radians)
    :param [in]: Vinf Freestream velocity
    :param [in]: span Hershey Bar full-span. Note, only half is used in the calculation
    :param [in]: full_span_flag Flag to apply symmetry to results
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: Theoretical coefficient of lift distribution array (size = 2*npts if full_span_flag = true)
    """
    return _vsp.GetHersheyBarLiftDist(npts, alpha, Vinf, span, full_span_flag)

@client_wrap
def GetHersheyBarDragDist(npts, alpha, Vinf, span, full_span_flag=False):
    r"""
    Get the theoretical drag (Cd) distribution for a Hershey Bar wing with unit chord length using Glauert's Method. This function was initially created to compare VSPAERO results to Lifting Line Theory.
    If full_span_flag is set to true symmetry is applied to the results.


    .. code-block:: python

        pi = 3.14159265358979323846
        # Compute theoretical lift and drag distributions using 100 points
        Vinf = 100

        halfAR = 20

        alpha_deg = 10

        n_pts = 100

        cl_dist_theo = GetHersheyBarLiftDist( int( n_pts ), alpha_deg*pi/180, Vinf, ( 2 * halfAR ), False )

        cd_dist_theo = GetHersheyBarDragDist( int( n_pts ), alpha_deg*pi/180, Vinf, ( 2 * halfAR ), False )


    :param [in]: npts Number of points along the span to assess
    :param [in]: alpha Wing angle of attack (Radians)
    :param [in]: Vinf Freestream velocity
    :param [in]: span Hershey Bar full-span. Note, only half is used in the calculation
    :param [in]: full_span_flag Flag to apply symmetry to results (default: false)
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: Theoretical coefficient of drag distribution array (size = 2*npts if full_span_flag = true)
    """
    return _vsp.GetHersheyBarDragDist(npts, alpha, Vinf, span, full_span_flag)

@client_wrap
def GetVKTAirfoilPnts(npts, alpha, epsilon, kappa, tau):
    r"""
    Get the 2D coordinates an input number of points along a Von K�rm�n-Trefftz airfoil of specified shape


    .. code-block:: python

        pi = 3.14159265358979323846

        npts = 122

        alpha = 0.0

        epsilon = 0.1

        kappa = 0.1

        tau = 10

        xyz_airfoil = GetVKTAirfoilPnts(npts, alpha, epsilon, kappa, tau*(pi/180) )

        cp_dist = GetVKTAirfoilCpDist( alpha, epsilon, kappa, tau*(pi/180), xyz_airfoil )


    :param [in]: npts Number of points along the airfoil to return
    :param [in]: alpha Airfoil angle of attack (Radians)
    :param [in]: epsilon Airfoil thickness
    :param [in]: kappa Airfoil camber
    :param [in]: tau Airfoil trailing edge angle (Radians)
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: Array of points on the VKT airfoil (size = npts)
    """
    return _vsp.GetVKTAirfoilPnts(npts, alpha, epsilon, kappa, tau)

@client_wrap
def GetVKTAirfoilCpDist(alpha, epsilon, kappa, tau, xyz_data):
    r"""
    Get the pressure coefficient (Cp) along a Von Kármán-Trefftz airfoil of specified shape at specified points along the airfoil


    .. code-block:: python

        pi = 3.14159265358979323846

        npts = 122

        alpha = 0.0

        epsilon = 0.1

        kappa = 0.1

        tau = 10

        xyz_airfoil = GetVKTAirfoilPnts(npts, alpha, epsilon, kappa, tau*(pi/180) )

        cp_dist = GetVKTAirfoilCpDist( alpha, epsilon, kappa, tau*(pi/180), xyz_airfoil )


    See also: GetVKTAirfoilPnts
    :param [in]: alpha double Airfoil angle of attack (Radians)
    :param [in]: epsilon double Airfoil thickness
    :param [in]: kappa double Airfoil camber
    :param [in]: tau double Airfoil trailing edge angle (Radians)
    :param [in]: xyz_data vector<vec3d> Vector of points on the airfoil to evaluate
    :rtype: std::vector< double,std::allocator< double > >
    :return: vector<double> Vector of Cp values for each point in xydata
    """
    return _vsp.GetVKTAirfoilCpDist(alpha, epsilon, kappa, tau, xyz_data)

@client_wrap
def GetEllipsoidSurfPnts(center, abc_rad, u_npts=20, w_npts=20):
    r"""
    Generate the surface coordinate points for a ellipsoid at specified center of input radius along each axis.
    Based on the MATLAB function ellipsoid (https://in.mathworks.com/help/matlab/ref/ellipsoid.html).
    See also: GetVKTAirfoilPnts
    :param [in]: center 3D location of the ellipsoid center
    :param [in]: abc_rad Radius along the A (X), B (Y), and C (Z) axes
    :param [in]: u_npts Number of points in the U direction
    :param [in]: w_npts Number of points in the W direction
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: Array of coordinates describing the ellipsoid surface
    """
    return _vsp.GetEllipsoidSurfPnts(center, abc_rad, u_npts, w_npts)

@client_wrap
def GetFeatureLinePnts(geom_id):
    r"""
    Get the points along the feature lines of a particular Geom
    :param [in]: geom_id string Geom ID
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: Array of points along the Geom's feature lines
    """
    return _vsp.GetFeatureLinePnts(geom_id)

@client_wrap
def GetEllipsoidCpDist(surf_pnt_vec, abc_rad, V_inf):
    r"""
    Generate Analytical Solution for Potential Flow for specified ellipsoid shape at input surface points for input velocity vector.
    Based on Munk, M. M., 'Remarks on the Pressure Distribution over the Surface of an Ellipsoid, Moving Translationally Through a Perfect
    Fluid,' NACA TN-196, June 1924. Function initially created to compare VSPAERO results to theory.


    .. code-block:: python

        import math
        pi = 3.14159265358979323846

        npts = 101

        abc_rad = vec3d(1.0, 2.0, 3.0)

        alpha = 5 # deg

        beta = 5 # deg

        V_inf = 100.0

        x_slice_pnt_vec = [None]*npts
        theta_vec = [None]*npts

        theta_vec[0] = 0

        for i in range(1, npts):
            theta_vec[i] = theta_vec[i-1] + (2 * pi / (npts - 1))


        for i in range(npts):

            x_slice_pnt_vec[i] = vec3d( 0, abc_rad.y() * math.cos( theta_vec[i] ), abc_rad.z() * math.sin( theta_vec[i] ) )

        V_vec = vec3d( ( V_inf * math.cos( alpha*pi/180 ) * math.cos( beta*pi/180 ) ), ( V_inf * math.sin( beta*pi/180 ) ), ( V_inf * math.sin( alpha*pi/180 ) * math.cos( beta*pi/180 ) ) )

        cp_dist = GetEllipsoidCpDist( x_slice_pnt_vec, abc_rad, V_vec )


    See also: GetEllipsoidSurfPnts
    :param [in]: surf_pnt_vec vector<vec3d> Vector of points on the ellipsoid surface to assess
    :param [in]: abc_rad vec3d Radius along the A (X), B (Y), and C (Z) axes
    :param [in]: V_inf vec3d 3D components of freestream velocity
    :rtype: std::vector< double,std::allocator< double > >
    :return: vector<double> Vector of Cp results corresponding to each point in surf_pnt_arr
    """
    return _vsp.GetEllipsoidCpDist(surf_pnt_vec, abc_rad, V_inf)

@client_wrap
def IntegrateEllipsoidFlow(abc_rad, abc_index):
    r"""IntegrateEllipsoidFlow(vec3d abc_rad, int const & abc_index) -> double"""
    return _vsp.IntegrateEllipsoidFlow(abc_rad, abc_index)

@client_wrap
def GetAirfoilUpperPnts(xsec_id):
    r"""
    Get the coordinate points for the upper surface of an airfoil. The XSec must be of type XS_FILE_AIRFOIL


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_FILE_AIRFOIL )

        xsec = GetXSec( xsec_surf, 1 )

        ReadFileAirfoil( xsec, "airfoil/N0012_VSP.af" )

        up_array = GetAirfoilUpperPnts( xsec )


    See also: SetAirfoilPnts
    :param [in]: xsec_id string XSec ID
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> VectorArray of coordinate points for the upper airfoil surface
    """
    return _vsp.GetAirfoilUpperPnts(xsec_id)

@client_wrap
def GetAirfoilLowerPnts(xsec_id):
    r"""
    Get the coordinate points for the lower surface of an airfoil. The XSec must be of type XS_FILE_AIRFOIL


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_FILE_AIRFOIL )

        xsec = GetXSec( xsec_surf, 1 )

        ReadFileAirfoil( xsec, "airfoil/N0012_VSP.af" )

        low_array = GetAirfoilLowerPnts( xsec )


    See also: SetAirfoilPnts
    :param [in]: xsec_id string XSec ID
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> Vector of coordinate points for the lower airfoil surface
    """
    return _vsp.GetAirfoilLowerPnts(xsec_id)

@client_wrap
def GetUpperCSTCoefs(xsec_id):
    r"""
    Get the CST coefficients for the upper surface of an airfoil. The XSec must be of type XS_CST_AIRFOIL
    See also: SetUpperCST
    :param [in]: xsec_id string XSec ID
    :rtype: std::vector< double,std::allocator< double > >
    :return: vector<double> Vector of CST coefficients for the upper airfoil surface
    """
    return _vsp.GetUpperCSTCoefs(xsec_id)

@client_wrap
def GetLowerCSTCoefs(xsec_id):
    r"""
    Get the CST coefficients for the lower surface of an airfoil. The XSec must be of type XS_CST_AIRFOIL
    See also: SetLowerCST
    :param [in]: xsec_id string XSec ID
    :rtype: std::vector< double,std::allocator< double > >
    :return: vector<double> Vector of CST coefficients for the lower airfoil surface
    """
    return _vsp.GetLowerCSTCoefs(xsec_id)

@client_wrap
def GetUpperCSTDegree(xsec_id):
    r"""
    Get the CST degree for the upper surface of an airfoil. The XSec must be of type XS_CST_AIRFOIL
    See also: SetUpperCST
    :param [in]: xsec_id string XSec ID
    :rtype: int
    :return: int CST Degree for upper airfoil surface
    """
    return _vsp.GetUpperCSTDegree(xsec_id)

@client_wrap
def GetLowerCSTDegree(xsec_id):
    r"""
    Get the CST degree for the lower surface of an airfoil. The XSec must be of type XS_CST_AIRFOIL
    See also: SetLowerCST
    :param [in]: xsec_id XSec ID
    :rtype: int
    :return: int CST Degree for lower airfoil surface
    """
    return _vsp.GetLowerCSTDegree(xsec_id)

@client_wrap
def SetUpperCST(xsec_id, deg, coefs):
    r"""
    Set the CST degree and coefficients for the upper surface of an airfoil. The number of coefficients should be one more than the CST degree. The XSec must be of type XS_CST_AIRFOIL
    See also: GetUpperCSTDegree, GetUpperCSTCoefs
    :param [in]: xsec_id string XSec ID
    :param [in]: deg int CST degree of upper airfoil surface
    :param [in]: coefs vector<double> Vector of CST coefficients for the upper airfoil surface
    """
    return _vsp.SetUpperCST(xsec_id, deg, coefs)

@client_wrap
def SetLowerCST(xsec_id, deg, coefs):
    r"""
    Set the CST degree and coefficients for the lower surface of an airfoil. The number of coefficients should be one more than the CST degree. The XSec must be of type XS_CST_AIRFOIL
    See also: GetLowerCSTDegree, GetLowerCSTCoefs
    :param [in]: xsec_id string XSec ID
    :param [in]: deg int CST degree of lower airfoil surface
    :param [in]: coefs vector<double> Vector of CST coefficients for the lower airfoil surface
    """
    return _vsp.SetLowerCST(xsec_id, deg, coefs)

@client_wrap
def PromoteCSTUpper(xsec_id):
    r"""
    Promote the CST for the upper airfoil surface. The XSec must be of type XS_CST_AIRFOIL
    See also: GetUpperCSTDegree
    :param [in]: xsec_id XSec ID
    """
    return _vsp.PromoteCSTUpper(xsec_id)

@client_wrap
def PromoteCSTLower(xsec_id):
    r"""
    Promote the CST for the lower airfoil surface. The XSec must be of type XS_CST_AIRFOIL
    See also: GetLowerCSTDegree
    :param [in]: xsec_id XSec ID
    """
    return _vsp.PromoteCSTLower(xsec_id)

@client_wrap
def DemoteCSTUpper(xsec_id):
    r"""
    Demote the CST for the upper airfoil surface. The XSec must be of type XS_CST_AIRFOIL
    See also: GetUpperCSTDegree
    :param [in]: xsec_id XSec ID
    """
    return _vsp.DemoteCSTUpper(xsec_id)

@client_wrap
def DemoteCSTLower(xsec_id):
    r"""
    Demote the CST for the lower airfoil surface. The XSec must be of type XS_CST_AIRFOIL
    See also: GetLowerCSTDegree
    :param [in]: xsec_id XSec ID
    """
    return _vsp.DemoteCSTLower(xsec_id)

@client_wrap
def FitAfCST(xsec_surf_id, xsec_index, deg):
    r"""
    Fit a CST airfoil for an existing airfoil of type XS_FOUR_SERIES, XS_SIX_SERIES, XS_FOUR_DIGIT_MOD, XS_FIVE_DIGIT, XS_FIVE_DIGIT_MOD, XS_ONE_SIX_SERIES, or XS_FILE_AIRFOIL.
    :param [in]: xsec_surf_id XsecSurf ID
    :param [in]: xsec_index XSec index
    :param [in]: deg CST degree
    """
    return _vsp.FitAfCST(xsec_surf_id, xsec_index, deg)

@client_wrap
def ChangeBORXSecShape(bor_id, type):
    r"""
    Set the XSec type for a BOR component


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_ROUNDED_RECTANGLE )

        if  GetBORXSecShape( bor_id ) != XS_ROUNDED_RECTANGLE : print( "ERROR: ChangeBORXSecShape" )


    See also: XSEC_CRV_TYPE
    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: type int XSec type enum (i.e. XS_ROUNDED_RECTANGLE)
    """
    return _vsp.ChangeBORXSecShape(bor_id, type)

@client_wrap
def GetBORXSecShape(bor_id):
    r"""
    Get the XSec type for a BOR component


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_ROUNDED_RECTANGLE )

        if  GetBORXSecShape( bor_id ) != XS_ROUNDED_RECTANGLE : print( "ERROR: GetBORXSecShape" )


    :param [in]: bor_id string Body of revolution Geom ID
    :rtype: int
    :return: int XSec type enum (i.e. XS_ROUNDED_RECTANGLE)
    """
    return _vsp.GetBORXSecShape(bor_id)

@client_wrap
def ReadBORFileXSec(bor_id, file_name):
    r"""
    Set the coordinate points for a specific BOR. The BOR XSecCurve must be of type XS_FILE_FUSE.


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_FILE_FUSE )

        vec_array = ReadBORFileXSec( bor_id, "TestXSec.fxs" )


    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: file_name string Fuselage XSec file name
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> Array of coordinate points read from the file and set to the XSec
    """
    return _vsp.ReadBORFileXSec(bor_id, file_name)

@client_wrap
def SetBORXSecPnts(bor_id, pnt_vec):
    r"""
    Set the coordinate points for a specific BOR. The BOR XSecCurve must be of type XS_FILE_FUSE.


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_FILE_FUSE )

        vec_array = ReadBORFileXSec( bor_id, "TestXSec.fxs" )

        if  len(vec_array) > 0 :
            vec_array[1] = vec_array[1] * 2.0
            vec_array[3] = vec_array[3] * 2.0

            SetBORXSecPnts( bor_id, vec_array )


    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: pnt_vec vector<vec3d> Vector of XSec coordinate points
    """
    return _vsp.SetBORXSecPnts(bor_id, pnt_vec)

@client_wrap
def ComputeBORXSecPnt(bor_id, fract):
    r"""
    Compute 3D coordinate for a point on a BOR XSecCurve given the parameter value (U) along the curve


    .. code-block:: python

        #==== Add Geom ====//
        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        u_fract = 0.25

        pnt = ComputeBORXSecPnt( bor_id, u_fract )


    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: fract double Curve parameter value (range: 0 - 1)
    :rtype: :py:class:`vec3d`
    :return: vec3d Coordinate point on curve
    """
    return _vsp.ComputeBORXSecPnt(bor_id, fract)

@client_wrap
def ComputeBORXSecTan(bor_id, fract):
    r"""
    Compute the tangent vector of a point on a BOR XSecCurve given the parameter value (U) along the curve


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        u_fract = 0.25

        tan = ComputeBORXSecTan( bor_id, u_fract )


    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: fract double Curve parameter value (range: 0 - 1)
    :rtype: :py:class:`vec3d`
    :return: vec3d Tangent vector on curve
    """
    return _vsp.ComputeBORXSecTan(bor_id, fract)

@client_wrap
def ReadBORFileAirfoil(bor_id, file_name):
    r"""
    Read in shape from airfoil file and set to the specified BOR XSecCurve. The XSecCurve must be of type XS_FILE_AIRFOIL. Airfoil files may be in Lednicer or Selig format with *.af or *.dat extensions.


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL )

        ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" )


    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: file_name string Airfoil XSec file name
    """
    return _vsp.ReadBORFileAirfoil(bor_id, file_name)

@client_wrap
def SetBORAirfoilUpperPnts(bor_id, up_pnt_vec):
    r"""
    Set the upper points for an airfoil on a BOR. The BOR XSecCurve must be of type XS_FILE_AIRFOIL.


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL )

        ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" )

        up_array = GetBORAirfoilUpperPnts( bor_id )

        for i in range(int( len(up_array) )):

            up_array[i].scale_y( 2.0 )

        SetBORAirfoilUpperPnts( bor_id, up_array )


    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: up_pnt_vec vector<vec3d> Vector of points defining the upper surface of the airfoil
    """
    return _vsp.SetBORAirfoilUpperPnts(bor_id, up_pnt_vec)

@client_wrap
def SetBORAirfoilLowerPnts(bor_id, low_pnt_vec):
    r"""
    Set the lower points for an airfoil on a BOR. The BOR XSecCurve must be of type XS_FILE_AIRFOIL.


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL )

        ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" )

        low_array = GetBORAirfoilLowerPnts( bor_id )

        for i in range(int( len(low_array) )):

            low_array[i].scale_y( 0.5 )

        SetBORAirfoilLowerPnts( bor_id, low_array )


    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: low_pnt_vec vector<vec3d> Vector of points defining the lower surface of the airfoil
    """
    return _vsp.SetBORAirfoilLowerPnts(bor_id, low_pnt_vec)

@client_wrap
def SetBORAirfoilPnts(bor_id, up_pnt_vec, low_pnt_vec):
    r"""
    Set the upper and lower points for an airfoil on a BOR. The BOR XSecCurve must be of type XS_FILE_AIRFOIL.


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL )

        ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" )

        up_array = GetBORAirfoilUpperPnts( bor_id )

        low_array = GetBORAirfoilLowerPnts( bor_id )

        for i in range(int( len(up_array) )):

            up_array[i].scale_y( 2.0 )

            low_array[i].scale_y( 0.5 )

        SetBORAirfoilPnts( bor_id, up_array, low_array )


    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: up_pnt_vec vector<vec3d> Vector of points defining the upper surface of the airfoil
    :param [in]: low_pnt_vec vector<_>vec3d> Vector of points defining the lower surface of the airfoil
    """
    return _vsp.SetBORAirfoilPnts(bor_id, up_pnt_vec, low_pnt_vec)

@client_wrap
def GetBORAirfoilUpperPnts(bor_id):
    r"""
    Get the coordinate points for the upper surface of an airfoil on a BOR. The BOR XSecCurve must be of type XS_FILE_AIRFOIL


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL )

        ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" )

        up_array = GetBORAirfoilUpperPnts( bor_id )


    See also: SetAirfoilPnts
    :param [in]: bor_id string Body of revolution Geom ID
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> Vector of coordinate points for the upper airfoil surface
    """
    return _vsp.GetBORAirfoilUpperPnts(bor_id)

@client_wrap
def GetBORAirfoilLowerPnts(bor_id):
    r"""
    Get the coordinate points for the lower surface of an airfoil of a BOR. The XSecCurve must be of type XS_FILE_AIRFOIL


    .. code-block:: python

        # Add Body of Recolution
        bor_id = AddGeom( "BODYOFREVOLUTION", "" )

        ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL )

        ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" )

        low_array = GetBORAirfoilLowerPnts( bor_id )


    See also: SetAirfoilPnts
    :param [in]: bor_id string Body of revolution Geom ID
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> Vector of coordinate points for the lower airfoil surface
    """
    return _vsp.GetBORAirfoilLowerPnts(bor_id)

@client_wrap
def GetBORUpperCSTCoefs(bor_id):
    r"""
    Get the CST coefficients for the upper surface of an airfoil of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: SetUpperCST
    :param [in]: bor_id Body of revolution Geom ID
    :rtype: std::vector< double,std::allocator< double > >
    :return: vector<double> Vector of CST coefficients for the upper airfoil surface
    """
    return _vsp.GetBORUpperCSTCoefs(bor_id)

@client_wrap
def GetBORLowerCSTCoefs(bor_id):
    r"""
    Get the CST coefficients for the lower surface of an airfoil of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: SetLowerCST
    :param [in]: bor_id string Body of revolution Geom ID
    :rtype: std::vector< double,std::allocator< double > >
    :return: vector<double> Vector of CST coefficients for the lower airfoil surface
    """
    return _vsp.GetBORLowerCSTCoefs(bor_id)

@client_wrap
def GetBORUpperCSTDegree(bor_id):
    r"""
    Get the CST degree for the upper surface of an airfoil of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: SetUpperCST
    :param [in]: bor_id string Body of revolution Geom ID
    :rtype: int
    :return: int CST Degree for upper airfoil surface
    """
    return _vsp.GetBORUpperCSTDegree(bor_id)

@client_wrap
def GetBORLowerCSTDegree(bor_id):
    r"""
    Get the CST degree for the lower surface of an airfoil of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: SetLowerCST
    :param [in]: bor_id string Body of revolution Geom ID
    :rtype: int
    :return: int CST Degree for lower airfoil surface
    """
    return _vsp.GetBORLowerCSTDegree(bor_id)

@client_wrap
def SetBORUpperCST(bor_id, deg, coefs):
    r"""
    Set the CST degree and coefficients for the upper surface of an airfoil of a BOR. The number of coefficients should be one more than the CST degree. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: GetUpperCSTDegree, GetUpperCSTCoefs
    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: deg CST degree of upper airfoil surface
    :param [in]: coefs Array of CST coefficients for the upper airfoil surface
    """
    return _vsp.SetBORUpperCST(bor_id, deg, coefs)

@client_wrap
def SetBORLowerCST(bor_id, deg, coefs):
    r"""
    Set the CST degree and coefficients for the lower surface of an airfoil of a BOR. The number of coefficients should be one more than the CST degree. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: GetLowerCSTDegree, GetLowerCSTCoefs
    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: deg int CST degree of lower airfoil surface
    :param [in]: coefs vector<double> Vector of CST coefficients for the lower airfoil surface
    """
    return _vsp.SetBORLowerCST(bor_id, deg, coefs)

@client_wrap
def PromoteBORCSTUpper(bor_id):
    r"""
    Promote the CST for the upper airfoil surface of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: GetUpperCSTDegree
    :param [in]: bor_id string Body of revolution Geom ID
    """
    return _vsp.PromoteBORCSTUpper(bor_id)

@client_wrap
def PromoteBORCSTLower(bor_id):
    r"""
    Promote the CST for the lower airfoil surface of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: GetLowerCSTDegree
    :param [in]: bor_id string Body of revolution Geom ID
    """
    return _vsp.PromoteBORCSTLower(bor_id)

@client_wrap
def DemoteBORCSTUpper(bor_id):
    r"""
    Demote the CST for the upper airfoil surface of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: GetUpperCSTDegree
    :param [in]: bor_id string Body of revolution Geom ID
    """
    return _vsp.DemoteBORCSTUpper(bor_id)

@client_wrap
def DemoteBORCSTLower(bor_id):
    r"""
    Demote the CST for the lower airfoil surface of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL
    See also: GetLowerCSTDegree
    :param [in]: bor_id string Body of revolution Geom ID
    """
    return _vsp.DemoteBORCSTLower(bor_id)

@client_wrap
def FitBORAfCST(bor_id, deg):
    r"""
    Fit a CST airfoil for an existing airfoil of a BOR of type XS_FOUR_SERIES, XS_SIX_SERIES, XS_FOUR_DIGIT_MOD, XS_FIVE_DIGIT, XS_FIVE_DIGIT_MOD, XS_ONE_SIX_SERIES, or XS_FILE_AIRFOIL.
    :param [in]: bor_id string Body of revolution Geom ID
    :param [in]: deg int CST degree
    """
    return _vsp.FitBORAfCST(bor_id, deg)

@client_wrap
def WriteBezierAirfoil(file_name, geom_id, foilsurf_u):
    r"""
    Write out the untwisted unit-length 2D Bezier curve for the specified airfoil in custom *.bz format. The output will describe the analytical shape of the airfoil. See BezierAirfoilExample.m and BezierCtrlToCoordPnts.m for examples of
    discretizing the Bezier curve and generating a Selig airfoil file.


    .. code-block:: python

        #==== Add Wing Geometry and Set Parms ====//
        wing_id = AddGeom( "WING", "" )

        u = 0.5 # export airfoil at mid span location

        #==== Write Bezier Airfoil File ====//
        WriteBezierAirfoil( "Example_Bezier.bz", wing_id, u )


    :param [in]: file_name Airfoil (*.bz) output file name
    :param [in]: geom_id string Geom ID
    :param [in]: foilsurf_u U location (range: 0 - 1) along the surface. The foil surface does not include root and tip caps (i.e. 2 section wing -> XSec0 @ u=0, XSec1 @ u=0.5, XSec2 @ u=1.0)
    """
    return _vsp.WriteBezierAirfoil(file_name, geom_id, foilsurf_u)

@client_wrap
def WriteSeligAirfoil(file_name, geom_id, foilsurf_u):
    r"""
    Write out the untwisted unit-length 2D coordinate points for the specified airfoil in Selig format. Coordinate points follow the on-screen wire frame W tessellation.


    .. code-block:: python

        #==== Add Wing Geometry and Set Parms ====//
        wing_id = AddGeom( "WING", "" )

        u = 0.5 # export airfoil at mid span location

        #==== Write Selig Airfoil File ====//
        WriteSeligAirfoil( "Example_Selig.dat", wing_id, u )


    See also: GetAirfoilCoordinates
    :param [in]: file_name Airfoil (*.dat) output file name
    :param [in]: geom_id string Geom ID
    :param [in]: foilsurf_u U location (range: 0 - 1) along the surface. The foil surface does not include root and tip caps (i.e. 2 section wing -> XSec0 @ u=0, XSec1 @ u=0.5, XSec2 @ u=1.0)
    """
    return _vsp.WriteSeligAirfoil(file_name, geom_id, foilsurf_u)

@client_wrap
def GetAirfoilCoordinates(geom_id, foilsurf_u):
    r"""
    Get the untwisted unit-length 2D coordinate points for the specified airfoil
    See also: WriteSeligAirfoil
    :param [in]: geom_id string Geom ID
    :param [in]: foilsurf_u U location (range: 0 - 1) along the surface. The foil surface does not include root and tip caps (i.e. 2 section wing -> XSec0 @ u=0, XSec1 @ u=0.5, XSec2 @ u=1.0)
    """
    return _vsp.GetAirfoilCoordinates(geom_id, foilsurf_u)

@client_wrap
def EditXSecInitShape(xsec_id):
    r"""
    Initialize the EditCurveXSec to the current value of m_ShapeType (i.e. EDIT_XSEC_ELLIPSE)


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 2, XS_EDIT_CURVE )

        # Identify XSec 2
        xsec_2 = GetXSec( xsec_surf, 2 )

        # Set XSec 2 to linear
        EditXSecConvertTo( xsec_2, LINEAR )

        EditXSecInitShape( xsec_2 ) # Change back to default ellipse


    See also: INIT_EDIT_XSEC_TYPE
    :param [in]: xsec_id XSec ID
    """
    return _vsp.EditXSecInitShape(xsec_id)

@client_wrap
def EditXSecConvertTo(xsec_id, newtype):
    r"""
    Convert the EditCurveXSec curve type to the specified new type. Note, EditCurveXSec uses the same enumerations for PCurve to identify curve type,
    but APPROX_CEDIT is not supported at this time.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_EDIT_CURVE )

        # Identify XSec 1
        xsec_1 = GetXSec( xsec_surf, 1 )

        # Set XSec 1 to Linear
        EditXSecConvertTo( xsec_1, LINEAR )


    See also: PCURV_TYPE
    :param [in]: xsec_id XSec ID
    :param [in]: newtype New curve type enum (i.e. CEDIT)
    """
    return _vsp.EditXSecConvertTo(xsec_id, newtype)

@client_wrap
def GetEditXSecUVec(xsec_id):
    r"""
    Get the U parameter vector for an EditCurveXSec. The vector will be in increasing order with a range of 0 - 1.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 2, XS_EDIT_CURVE )

        # Identify XSec 2
        xsec_2 = GetXSec( xsec_surf, 2 )

        # Set XSec 2 to linear
        EditXSecConvertTo( xsec_2, LINEAR )

        u_vec = GetEditXSecUVec( xsec_2 )

        if  u_vec[1] - 0.25 > 1e-6 :
            print( "Error: GetEditXSecUVec" )


    :param [in]: xsec_id XSec ID
    :rtype: std::vector< double,std::allocator< double > >
    :return: Array of U parameter values
    """
    return _vsp.GetEditXSecUVec(xsec_id)

@client_wrap
def GetEditXSecCtrlVec(xsec_id, non_dimensional=True):
    r"""
    Get the control point vector for an EditCurveXSec. Note, the returned array of vec3d values will be represented in 2D with Z set to 0.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_EDIT_CURVE )

        # Identify XSec 1
        xsec_1 = GetXSec( xsec_surf, 1 )

        # Get the control points for the default shape
        xsec1_pts = GetEditXSecCtrlVec( xsec_1, True ) # The returned control points will not be scaled by width and height

        print( f"Normalized Bottom Point of XSecCurve: {xsec1_pts[3].x()}, {xsec1_pts[3].y()}, {xsec1_pts[3].z()}" )


    :param [in]: xsec_id XSec ID
    :param [in]: non_dimensional True to get the points non-dimensionalized, False to get them scaled by m_Width and m_Height
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: Array of control points
    """
    return _vsp.GetEditXSecCtrlVec(xsec_id, non_dimensional)

@client_wrap
def SetEditXSecPnts(xsec_id, u_vec, control_pts, r_vec):
    r"""
    Set the U parameter vector and the control point vector for an EditCurveXSec. The arrays must be of equal length, with the values for U defined in
    increasing order and range 0 - 1. The input control points to SetEditXSecPnts must be nondimensionalized in the approximate range of [-0.5, 0.5].


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 2, XS_EDIT_CURVE )

        # Identify XSec 2
        xsec_2 = GetXSec( xsec_surf, 2 )

        # Set XSec 2 to linear
        EditXSecConvertTo( xsec_2, LINEAR )

        # Turn off R/L symmetry
        SetParmVal( GetXSecParm( xsec_2, "SymType"), SYM_NONE )

        # Define a square
        xsec2_pts = [vec3d(0.5, 0.5, 0.0),
                 vec3d(0.5, -0.5, 0.0),
                 vec3d(-0.5, -0.5, 0.0),
                 vec3d(-0.5, 0.5, 0.0),
                 vec3d(0.5, 0.5, 0.0)]

        # u vec must start at 0.0 and end at 1.0
        u_vec = [0.0, 0.25, 0.5, 0.75, 1.0]

        r_vec = [0.0, 0.0, 0.0, 0.0, 0.0]

        SetEditXSecPnts( xsec_2, u_vec, xsec2_pts, r_vec ) # Note: points are unscaled by the width and height parms

        new_pnts = GetEditXSecCtrlVec( xsec_2, True ) # The returned control points will not be scaled by width and height

        if  dist( new_pnts[3], xsec2_pts[3] ) > 1e-6 :
            print( "Error: SetEditXSecPnts")


    :param [in]: xsec_id XSec ID
    :param [in]: u_vec Array of U parameter values
    :param [in]: r_vec Array of R parameter values
    :param [in]: control_pts Nondimensionalized array of control points
    """
    return _vsp.SetEditXSecPnts(xsec_id, u_vec, control_pts, r_vec)

@client_wrap
def EditXSecDelPnt(xsec_id, indx):
    r"""
    Delete an EditCurveXSec control point. Note, cubic Bezier intermediate control points (those not on the curve) cannot be deleted.
    The previous and next Bezier control point will be deleted along with the point on the curve. Regardless of curve type, the first
    and last points may not be deleted.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 2, XS_EDIT_CURVE )

        # Identify XSec 2
        xsec_2 = GetXSec( xsec_surf, 2 )

        # Turn off R/L symmetry
        SetParmVal( GetXSecParm( xsec_2, "SymType"), SYM_NONE )

        old_pnts = GetEditXSecCtrlVec( xsec_2, True ) # The returned control points will not be scaled by width and height

        EditXSecDelPnt( xsec_2, 3 ) # Remove control point at bottom of circle

        new_pnts = GetEditXSecCtrlVec( xsec_2, True ) # The returned control points will not be scaled by width and height

        if  len(old_pnts) - len(new_pnts) != 3  :
            print( "Error: EditXSecDelPnt")


    :param [in]: xsec_id XSec ID
    :param [in]: indx Control point index
    """
    return _vsp.EditXSecDelPnt(xsec_id, indx)

@client_wrap
def EditXSecSplit01(xsec_id, u):
    r"""
    Split the EditCurveXSec at the specified U value


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 2, XS_EDIT_CURVE )

        # Identify XSec 2
        xsec_2 = GetXSec( xsec_surf, 2 )

        # Turn off R/L symmetry
        SetParmVal( GetXSecParm( xsec_2, "SymType"), SYM_NONE )

        old_pnts = GetEditXSecCtrlVec( xsec_2, True ) # The returned control points will not be scaled by width and height

        new_pnt_ind = EditXSecSplit01( xsec_2, 0.375 )

        new_pnts = GetEditXSecCtrlVec( xsec_2, True ) # The returned control points will not be scaled by width and height

        if  len(new_pnts) - len(old_pnts) != 3  :
            print( "Error: EditXSecSplit01")


    :param [in]: xsec_id XSec ID
    :param [in]: u U value to split the curve at (0 - 1)
    :rtype: int
    :return: Index of the point added from the split
    """
    return _vsp.EditXSecSplit01(xsec_id, u)

@client_wrap
def MoveEditXSecPnt(xsec_id, indx, new_pnt):
    r"""
    Move an EditCurveXSec control point. The XSec points are nondimensionalized by m_Width and m_Height and
    defined in 2D, so the Z value of the new coordinate point will be ignored.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_EDIT_CURVE )

        # Identify XSec 1
        xsec_1 = GetXSec( xsec_surf, 1 )

        # Turn off R/L symmetry
        SetParmVal( GetXSecParm( xsec_1, "SymType"), SYM_NONE )

        # Get the control points for the default shape
        xsec1_pts = GetEditXSecCtrlVec( xsec_1, True ) # The returned control points will not be scaled by width and height

        # Identify a control point that lies on the curve and shift it in Y
        move_pnt_ind = 3

        new_pnt = vec3d( xsec1_pts[move_pnt_ind].x(), 2 * xsec1_pts[move_pnt_ind].y(), 0.0 )

        # Move the control point
        MoveEditXSecPnt( xsec_1, move_pnt_ind, new_pnt )

        new_pnts = GetEditXSecCtrlVec( xsec_1, True ) # The returned control points will not be scaled by width and height

        if  dist( new_pnt, new_pnts[move_pnt_ind] ) > 1e-6 :
            print( "Error: MoveEditXSecPnt" )


    :param [in]: xsec_id XSec ID
    :param [in]: indx Control point index
    :param [in]: new_pnt Coordinate of the new point
    """
    return _vsp.MoveEditXSecPnt(xsec_id, indx, new_pnt)

@client_wrap
def ConvertXSecToEdit(geom_id, indx=0):
    r"""
    Convert any XSec type into an EditCurveXSec. This function will work for BOR Geoms, in which case the input XSec index is ignored.


    .. code-block:: python

        # Add Stack
        sid = AddGeom( "STACK", "" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( sid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_ROUNDED_RECTANGLE )

        # Convert Rounded Rectangle to Edit Curve type XSec
        ConvertXSecToEdit( sid, 1 )

        # Identify XSec 1
        xsec_1 = GetXSec( xsec_surf, 1 )

        # Get the control points for the default shape
        xsec1_pts = GetEditXSecCtrlVec( xsec_1, True ) # The returned control points will not be scaled by width and height


    :param [in]: geom_id string Geom ID
    :param [in]: indx XSec index
    """
    return _vsp.ConvertXSecToEdit(geom_id, indx)

@client_wrap
def GetEditXSecFixedUVec(xsec_id):
    r"""
    Get the vector of fixed U flags for each control point in an EditCurveXSec. The fixed U flag is used to hold the
    U parameter of the control point constant when performing an equal arc length reparameterization of the curve.


    .. code-block:: python

        # Add Wing
        wid = AddGeom( "WING" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( wid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_EDIT_CURVE )

        # Identify XSec 1
        xsec_1 = GetXSec( xsec_surf, 1 )

        fixed_u_vec = list(GetEditXSecFixedUVec( xsec_1 ))

        fixed_u_vec[3] = True # change a flag

        SetEditXSecFixedUVec( xsec_1, fixed_u_vec )

        ReparameterizeEditXSec( xsec_1 )


    See also: SetEditXSecFixedUVec, ReparameterizeEditXSec
    :param [in]: xsec_id XSec ID
    :rtype: std::vector< bool,std::allocator< bool > >
    :return: Array of bool values for each control point
    """
    return _vsp.GetEditXSecFixedUVec(xsec_id)

@client_wrap
def SetEditXSecFixedUVec(xsec_id, fixed_u_vec):
    r"""
    Set the vector of fixed U flags for each control point in an EditCurveXSec. The fixed U flag is used to hold the
    U parameter of the control point constant when performing an equal arc length reparameterization of the curve.


    .. code-block:: python

        # Add Wing
        wid = AddGeom( "WING" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( wid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_EDIT_CURVE )

        # Identify XSec 1
        xsec_1 = GetXSec( xsec_surf, 1 )

        fixed_u_vec = list(GetEditXSecFixedUVec( xsec_1 ))

        fixed_u_vec[3] = True # change a flag

        SetEditXSecFixedUVec( xsec_1, fixed_u_vec )

        ReparameterizeEditXSec( xsec_1 )


    See also: GetEditXSecFixedUVec, ReparameterizeEditXSec
    :param [in]: xsec_id XSec ID
    :param [in]: fixed_u_vec Array of fixed U flags
    """
    return _vsp.SetEditXSecFixedUVec(xsec_id, fixed_u_vec)

@client_wrap
def ReparameterizeEditXSec(xsec_id):
    r"""
    Perform an equal arc length repareterization on an EditCurveXSec. The reparameterization is performed between
    specific U values if the Fixed U flag is true. This allows corners, such as at 0.25, 0.5, and 0.75 U, to be held
    constant while everything between them is reparameterized.


    .. code-block:: python

        # Add Wing
        wid = AddGeom( "WING" )

        # Get First (and Only) XSec Surf
        xsec_surf = GetXSecSurf( wid, 0 )

        ChangeXSecShape( xsec_surf, 1, XS_EDIT_CURVE )

        # Identify XSec 1
        xsec_1 = GetXSec( xsec_surf, 1 )

        fixed_u_vec = list(GetEditXSecFixedUVec( xsec_1 ))

        fixed_u_vec[3] = True # change a flag

        SetEditXSecFixedUVec( xsec_1, fixed_u_vec )

        ReparameterizeEditXSec( xsec_1 )


    See also: SetEditXSecFixedUVec, GetEditXSecFixedUVec
    :param [in]: xsec_id XSec ID
    """
    return _vsp.ReparameterizeEditXSec(xsec_id)

@client_wrap
def GetNumSets():
    r"""
    Get the total number of defined sets. Named sets are used to group components and read/write on them. The number of named
    sets will be 10 for OpenVSP versions up to 3.17.1 and 20 for later versions.


    .. code-block:: python

        if  GetNumSets() <= 0 : print( "---> Error: API GetNumSets " )


    :rtype: int
    :return: Number of sets
    """
    return _vsp.GetNumSets()

@client_wrap
def SetSetName(index, name):
    r"""
    Set the name of a set at specified index


    .. code-block:: python

        SetSetName( 3, "SetFromScript" )

        if GetSetName(3) != "SetFromScript":
            print("---> Error: API Get/Set Set Name")



    See also: SET_TYPE
    :param [in]: index Set index
    :param [in]: name Set name
    """
    return _vsp.SetSetName(index, name)

@client_wrap
def GetSetName(index):
    r"""
    Get the name of a set at specified index


    .. code-block:: python

        SetSetName( 3, "SetFromScript" )

        if GetSetName(3) != "SetFromScript":
            print("---> Error: API Get/Set Set Name")


    See also: SET_TYPE
    :param [in]: index Set index
    :rtype: string
    :return: Set name
    """
    return _vsp.GetSetName(index)

@client_wrap
def GetGeomSetAtIndex(index):
    r"""
    Get an array of Geom IDs for the specified set index


    .. code-block:: python

        SetSetName( 3, "SetFromScript" )

        geom_arr1 = GetGeomSetAtIndex( 3 )

        geom_arr2 = GetGeomSet( "SetFromScript" )

        if  len(geom_arr1) != len(geom_arr2) : print( "---> Error: API GetGeomSet " )


    See also: SET_TYPE
    :param [in]: index Set index
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Geom IDs
    """
    return _vsp.GetGeomSetAtIndex(index)

@client_wrap
def GetGeomSet(name):
    r"""
    Get an array of Geom IDs for the specified set name


    .. code-block:: python

        SetSetName( 3, "SetFromScript" )

        geom_arr1 = GetGeomSetAtIndex( 3 )

        geom_arr2 = GetGeomSet( "SetFromScript" )

        if  len(geom_arr1) != len(geom_arr2) : print( "---> Error: API GetGeomSet " )


    :param [in]: name const string set name
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: array<string> array of Geom IDs
    """
    return _vsp.GetGeomSet(name)

@client_wrap
def GetSetIndex(name):
    r"""
    Get the set index for the specified set name


    .. code-block:: python

        SetSetName( 3, "SetFromScript" )

        if GetSetIndex("SetFromScript") != 3:
            print("ERROR: GetSetIndex")



    :param [in]: name Set name
    :rtype: int
    :return: Set index
    """
    return _vsp.GetSetIndex(name)

@client_wrap
def GetSetFlag(geom_id, set_index):
    r"""
    Check if a Geom is in the set at the specified set index


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        SetSetFlag( fuseid, 3, True )

        if not GetSetFlag(fuseid, 3):
            print("---> Error: API Set/Get Set Flag")



    :param [in]: geom_id string Geom ID
    :param [in]: set_index Set index
    :rtype: boolean
    :return: True if geom is in the set, false otherwise
    """
    return _vsp.GetSetFlag(geom_id, set_index)

@client_wrap
def SetSetFlag(geom_id, set_index, flag):
    r"""
    Set whether or not a Geom is a member of the set at specified set index


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        SetSetFlag( fuseid, 3, True )

        if not GetSetFlag(fuseid, 3):
            print("---> Error: API Set/Get Set Flag")



    :param [in]: geom_id string Geom ID
    :param [in]: set_index Set index
    :param [in]: flag Flag that indicates set membership
    """
    return _vsp.SetSetFlag(geom_id, set_index, flag)

@client_wrap
def CopyPasteSet(copyIndex, pasteIndex):
    r"""
    Copies all the states of a geom set and pastes them into a specific set based on passed in indexs


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        #set fuseid's state for set 3 to true
        SetSetFlag( fuseid, 3, True )

        #Copy set 3 and Paste into set 4
        CopyPasteSet( 3, 4 )

        #get fuseid's state for set 4
        flag_value = GetSetFlag( fuseid, 4 )

        if  flag_value != True: print( "---> Error: API CopyPasteSet " )


    :param [in]: copyIndex Copy Index
    :param [in]: pasteIndex Paste Index
    """
    return _vsp.CopyPasteSet(copyIndex, pasteIndex)

@client_wrap
def ScaleSet(set_index, scale):
    r"""
    Apply a scale factor to a set


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE" )

        SetSetFlag( fuseid, 3, True )

        # Scale by a factor of 2
        ScaleSet( 3, 2.0 )


    :param [in]: set_index Set index
    :param [in]: scale Scale factor
    """
    return _vsp.ScaleSet(set_index, scale)

@client_wrap
def RotateSet(set_index, x_rot_deg, y_rot_deg, z_rot_deg):
    r"""
    Rotate a set about the global X, Y, and Z axes


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE" )

        SetSetFlag( fuseid, 3, True )

        # Rotate 90 degrees about Y
        RotateSet( 3, 0, 90, 0 )


    :param [in]: set_index Set index
    :param [in]: x_rot_deg Rotation about the X axis (degrees)
    :param [in]: y_rot_deg Rotation about the Y axis (degrees)
    :param [in]: z_rot_deg Rotation about the Z axis (degrees)
    """
    return _vsp.RotateSet(set_index, x_rot_deg, y_rot_deg, z_rot_deg)

@client_wrap
def TranslateSet(set_index, translation_vec):
    r"""
    Translate a set along a given vector


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE" )

        SetSetFlag( fuseid, 3, True )

        # Translate 2 units in X and 3 units in Y
        TranslateSet( 3, vec3d( 2, 3, 0 ) )


    :param [in]: set_index Set index
    :param [in]: translation_vec Translation vector
    """
    return _vsp.TranslateSet(set_index, translation_vec)

@client_wrap
def TransformSet(set_index, translation_vec, x_rot_deg, y_rot_deg, z_rot_deg, scale, scale_translations_flag):
    r"""
    Apply translation, rotation, and scale transformations to a set


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE" )

        SetSetFlag( fuseid, 3, True )

        # Translate 2 units in X and 3 units in Y, rotate 90 degrees about Y, and scale by a factor of 2
        TransformSet( 3, vec3d( 2, 3, 0 ), 0, 90, 0, 2.0, True )


    See also: TranslateSet, RotateSet, ScaleSet
    :param [in]: set_index Set index
    :param [in]: translation_vec Translation vector
    :param [in]: x_rot_deg Rotation about the X axis (degrees)
    :param [in]: y_rot_deg Rotation about the Y axis (degrees)
    :param [in]: z_rot_deg Rotation about the Z axis (degrees)
    :param [in]: scale Scale factor
    :param [in]: scale_translations_flag Flag to apply the scale factor to translations
    """
    return _vsp.TransformSet(set_index, translation_vec, x_rot_deg, y_rot_deg, z_rot_deg, scale, scale_translations_flag)

@client_wrap
def ValidParm(id):
    r"""
    Check if given Parm is valid


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pid = AddGeom( "POD" )

        lenid = GetParm( pid, "Length", "Design" )

        if  not ValidParm( lenid ) : print( "---> Error: API GetParm  " )


    :param [in]: id Parm ID
    :rtype: boolean
    :return: True if Parm ID is valid, false otherwise
    """
    return _vsp.ValidParm(id)

@client_wrap
def SetParmVal(*args):
    r"""
    *Overload 1:*



    Set the value of the specified Parm.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        SetParmVal( wid, 23.0 )

        if  abs( GetParmVal( wid ) - 23 ) > 1e-6 : print( "---> Error: API Parm Val Set/Get " )


    See also: SetParmValUpdate
    :param [in]: parm_id string Parm ID
    :param [in]: val Parm value to set
    :rtype: float
    :return: Value that the Parm was set to


    |

    *Overload 2:*



    Set the value of the specified Parm.


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        SetParmVal( wid, 23.0 )

        if  abs( GetParmVal( wid ) - 23 ) > 1e-6 : print( "---> Error: API Parm Val Set/Get " )


    See also: SetParmValUpdate
    :param [in]: geom_id string Geom ID
    :param [in]: name string Parm name
    :param [in]: group string Parm group name
    :param [in]: val double Parm value to set
    :rtype: float
    :return: double Value that the Parm was set to
    """
    return _vsp.SetParmVal(*args)

@client_wrap
def SetParmValLimits(parm_id, val, lower_limit, upper_limit):
    r"""
    Set the value along with the upper and lower limits of the specified Parm


    .. code-block:: python

        pod_id = AddGeom( "POD" )

        length = FindParm( pod_id, "Length", "Design" )

        SetParmValLimits( length, 10.0, 0.001, 1.0e12 )

        SetParmDescript( length, "Total Length of Geom" )


    See also: SetParmLowerLimit, SetParmUpperLimit
    :param [in]: parm_id string Parm ID
    :param [in]: val Parm value to set
    :param [in]: lower_limit Parm lower limit
    :param [in]: upper_limit Parm upper limit
    :rtype: float
    :return: Value that the Parm was set to
    """
    return _vsp.SetParmValLimits(parm_id, val, lower_limit, upper_limit)

@client_wrap
def SetParmValUpdate(*args):
    r"""
    *Overload 1:*



    Set the value of the specified Parm and force an Update.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        parm_id = GetParm( pod_id, "X_Rel_Location", "XForm" )

        SetParmValUpdate( parm_id, 5.0 )


    See also: SetParmVal
    :param [in]: parm_id string Parm ID
    :param [in]: val Parm value to set
    :rtype: float
    :return: Value that the Parm was set to


    |

    *Overload 2:*



    Set the value of the specified Parm and force an Update.


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        parm_id = GetParm( pod_id, "X_Rel_Location", "XForm" )

        SetParmValUpdate( parm_id, 5.0 )


    See also: SetParmVal
    :param [in]: geom_id string Geom ID
    :param [in]: parm_name string Parm name
    :param [in]: parm_group_name string Parm group name
    :param [in]: val double Parm value to set
    :rtype: float
    :return: double Value that the Parm was set to
    """
    return _vsp.SetParmValUpdate(*args)

@client_wrap
def GetParmVal(*args):
    r"""
    *Overload 1:*



    Get the value of the specified Parm. The data type of the Parm value will be cast to a double


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        SetParmVal( wid, 23.0 )

        if  abs( GetParmVal( wid ) - 23 ) > 1e-6 : print( "---> Error: API Parm Val Set/Get " )


    :param [in]: parm_id string Parm ID
    :rtype: float
    :return: Parm value


    |

    *Overload 2:*



    Get the value of the specified Parm. The data type of the Parm value will be cast to a double


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        SetParmVal( wid, 23.0 )

        if  abs( GetParmVal( wid ) - 23 ) > 1e-6 : print( "---> Error: API Parm Val Set/Get " )


    :param [in]: geom_id string Geom ID
    :param [in]: name string Parm name
    :param [in]: group string Parm group name
    :rtype: float
    :return: double Parm value
    """
    return _vsp.GetParmVal(*args)

@client_wrap
def GetIntParmVal(parm_id):
    r"""
    Get the value of the specified int type Parm


    .. code-block:: python

        #==== Add Prop Geometry ====//
        prop_id = AddGeom( "PROP" )

        num_blade_id = GetParm( prop_id, "NumBlade", "Design" )

        num_blade = GetIntParmVal( num_blade_id )


    :param [in]: parm_id string Parm ID
    :rtype: int
    :return: double Parm value
    """
    return _vsp.GetIntParmVal(parm_id)

@client_wrap
def GetBoolParmVal(parm_id):
    r"""
    Get the value of the specified bool type Parm


    .. code-block:: python

        #==== Add Prop Geometry ====//
        prop_id = AddGeom( "PROP" )

        rev_flag_id = GetParm( prop_id, "ReverseFlag", "Design" )

        reverse_flag = GetBoolParmVal( rev_flag_id )


    :param [in]: parm_id string Parm ID
    :rtype: boolean
    :return: bool Parm value
    """
    return _vsp.GetBoolParmVal(parm_id)

@client_wrap
def SetParmUpperLimit(parm_id, val):
    r"""
    Set the upper limit value for the specified Parm


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        SetParmVal( wid, 23.0 )

        SetParmUpperLimit( wid, 13.0 )

        if  abs( GetParmVal( wid ) - 13 ) > 1e-6 : print( "---> Error: API SetParmUpperLimit " )


    See also: SetParmValLimits
    :param [in]: parm_id string Parm ID
    :param [in]: val double Parm upper limit
    """
    return _vsp.SetParmUpperLimit(parm_id, val)

@client_wrap
def GetParmUpperLimit(parm_id):
    r"""
    Get the upper limit value for the specified Parm


    .. code-block:: python

        #==== Add Prop Geometry ====//
        prop_id = AddGeom( "PROP" )

        num_blade_id = GetParm( prop_id, "NumBlade", "Design" )

        max_blade = GetParmUpperLimit( num_blade_id )


    :param [in]: parm_id string Parm ID
    :rtype: float
    :return: double Parm upper limit
    """
    return _vsp.GetParmUpperLimit(parm_id)

@client_wrap
def SetParmLowerLimit(parm_id, val):
    r"""
    Set the lower limit value for the specified Parm


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        SetParmVal( wid, 13.0 )

        SetParmLowerLimit( wid, 15.0 )

        if  abs( GetParmVal( wid ) - 15 ) > 1e-6 : print( "---> Error: API SetParmLowerLimit " )


    See also: SetParmValLimits
    :param [in]: parm_id string Parm ID
    :param [in]: val Parm lower limit
    """
    return _vsp.SetParmLowerLimit(parm_id, val)

@client_wrap
def GetParmLowerLimit(parm_id):
    r"""
    Get the lower limit value for the specified Parm


    .. code-block:: python

        #==== Add Prop Geometry ====//
        prop_id = AddGeom( "PROP" )

        num_blade_id = GetParm( prop_id, "NumBlade", "Design" )

        min_blade = GetParmLowerLimit( num_blade_id )


    :param [in]: parm_id string Parm ID
    :rtype: float
    :return: Parm lower limit
    """
    return _vsp.GetParmLowerLimit(parm_id)

@client_wrap
def GetParmType(parm_id):
    r"""
    Get the data type for the specified Parm


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        if  GetParmType( wid ) != PARM_DOUBLE_TYPE : print( "---> Error: API GetParmType " )


    See also: PARM_TYPE
    :param [in]: parm_id string Parm ID
    :rtype: int
    :return: Parm data type enum (i.e. PARM_BOOL_TYPE)
    """
    return _vsp.GetParmType(parm_id)

@client_wrap
def GetParmName(parm_id):
    r"""
    Get the name for the specified Parm


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Get Structure Name and Parm Container ID ====//
        parm_container_name = GetFeaStructName( pod_id, struct_ind )

        parm_container_id = FindContainer( parm_container_name, struct_ind )

        #==== Get and List All Parms in the Container ====//
        parm_ids = FindContainerParmIDs( parm_container_id )

        for i in range(len(parm_ids)):

            name_id = GetParmName( parm_ids[i] ) + ": " + parm_ids[i] + "\n"

            print( name_id )


    :param [in]: parm_id string Parm ID
    :rtype: string
    :return: Parm name
    """
    return _vsp.GetParmName(parm_id)

@client_wrap
def GetParmGroupName(parm_id):
    r"""
    Get the group name for the specified Parm


    .. code-block:: python

        veh_id = FindContainer( "Vehicle", 0 )

        #==== Get and List All Parms in the Container ====//
        parm_ids = FindContainerParmIDs( veh_id )

        print( "Parm Groups and IDs in Vehicle Parm Container: " )

        for i in range(len(parm_ids)):

            group_str = GetParmGroupName( parm_ids[i] ) + ": " + parm_ids[i] + "\n"

            print( group_str )


    :param [in]: parm_id string Parm ID
    :rtype: string
    :return: Parm group name
    """
    return _vsp.GetParmGroupName(parm_id)

@client_wrap
def GetParmDisplayGroupName(parm_id):
    r"""
    Get the display group name for the specified Parm


    .. code-block:: python

        veh_id = FindContainer( "Vehicle", 0 )

        #==== Get and List All Parms in the Container ====//
        parm_ids = FindContainerParmIDs( veh_id )

        print( "Parm Group Display Names and IDs in Vehicle Parm Container: " )

        for i in range(len(parm_ids)):

            group_str = GetParmDisplayGroupName( parm_ids[i] ) + ": " + parm_ids[i] + "\n"

            print( group_str )


    :param [in]: parm_id string Parm ID
    :rtype: string
    :return: Parm display group name
    """
    return _vsp.GetParmDisplayGroupName(parm_id)

@client_wrap
def GetParmContainer(parm_id):
    r"""
    Get Parm Container ID for the specified Parm


    .. code-block:: python

        # Add Fuselage Geom
        fuseid = AddGeom( "FUSELAGE", "" )

        xsec_surf = GetXSecSurf( fuseid, 0 )

        ChangeXSecShape( xsec_surf, GetNumXSec( xsec_surf ) - 1, XS_ROUNDED_RECTANGLE )

        xsec = GetXSec( xsec_surf, GetNumXSec( xsec_surf ) - 1 )

        wid = GetXSecParm( xsec, "RoundedRect_Width" )

        cid = GetParmContainer( wid )

        if  len(cid) == 0 : print( "---> Error: API GetParmContainer " )


    :param [in]: parm_id string Parm ID
    :rtype: string
    :return: Parm Container ID
    """
    return _vsp.GetParmContainer(parm_id)

@client_wrap
def SetParmDescript(parm_id, desc):
    r"""
    Set the description of the specified Parm


    .. code-block:: python

        pod_id = AddGeom( "POD" )

        length = FindParm( pod_id, "Length", "Design" )

        SetParmValLimits( length, 10.0, 0.001, 1.0e12 )

        SetParmDescript( length, "Total Length of Geom" )


    :param [in]: parm_id string Parm ID
    :param [in]: desc Parm description
    """
    return _vsp.SetParmDescript(parm_id, desc)

@client_wrap
def GetParmDescript(parm_id):
    r"""
    Get the description of the specified Parm


    .. code-block:: python

        pod_id = AddGeom( "POD" )

        length = FindParm( pod_id, "Length", "Design" )

        SetParmValLimits( length, 10.0, 0.001, 1.0e12 )

        desc = GetParmDescript( length )
        print( desc )


    :param [in]: parm_id string Parm ID
    :rtype: string
    :return: desc Parm description
    """
    return _vsp.GetParmDescript(parm_id)

@client_wrap
def FindParm(parm_container_id, parm_name, group_name):
    r"""
    Find a Parm ID given the Parm Container ID, Parm name, and Parm group


    .. code-block:: python

        #==== Add Wing Geometry ====//
        wing_id = AddGeom( "WING" )

        #==== Turn Symmetry OFF ====//
        sym_id = FindParm( wing_id, "Sym_Planar_Flag", "Sym")

        SetParmVal( sym_id, 0.0 ) # Note: bool input not supported in SetParmVal


    :param [in]: parm_container_id Parm Container ID
    :param [in]: parm_name Parm name
    :param [in]: group_name Parm group name
    :rtype: string
    :return: Parm ID
    """
    return _vsp.FindParm(parm_container_id, parm_name, group_name)

@client_wrap
def FindContainers():
    r"""
    Get an array of all Parm Container IDs


    .. code-block:: python

        ctr_arr = FindContainers()

        print( "---> API Parm Container IDs: " )

        for i in range(int( len(ctr_arr) )):

            message = "\t" + ctr_arr[i] + "\n"

            print( message )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Parm Container IDs
    """
    return _vsp.FindContainers()

@client_wrap
def FindContainersWithName(name):
    r"""
    Get an array of Parm Container IDs for Containers with the specified name


    .. code-block:: python

        ctr_arr = FindContainersWithName( "UserParms" )

        if  len(ctr_arr) > 0 : print( ( "UserParms Parm Container ID: " + ctr_arr[0] ) )


    :param [in]: name Parm Container name
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Parm Container IDs
    """
    return _vsp.FindContainersWithName(name)

@client_wrap
def FindContainer(name, index):
    r"""
    Get the ID of a Parm Container with specified name at input index


    .. code-block:: python

        #===== Get Vehicle Parm Container ID ====//
        veh_id = FindContainer( "Vehicle", 0 )


    See also: FindContainersWithName
    :param [in]: name Parm Container name
    :param [in]: index Parm Container index
    :rtype: string
    :return: Parm Container ID
    """
    return _vsp.FindContainer(name, index)

@client_wrap
def GetContainerName(parm_container_id):
    r"""
    Get the name of the specified Parm Container


    .. code-block:: python

        veh_id = FindContainer( "Vehicle", 0 )

        if  GetContainerName( veh_id) != "Vehicle":       print( "---> Error: API GetContainerName" )


    :param [in]: parm_container_id Parm Container ID
    :rtype: string
    :return: Parm Container name
    """
    return _vsp.GetContainerName(parm_container_id)

@client_wrap
def FindContainerGroupNames(parm_container_id):
    r"""
    Get an array of Parm group names included in the specified Container


    .. code-block:: python

        user_ctr = FindContainer( "UserParms", 0 )

        grp_arr = FindContainerGroupNames( user_ctr )

        print( "---> UserParms Container Group IDs: " )
        for i in range(int( len(grp_arr) )):

            message = "\t" + grp_arr[i] + "\n"

            print( message )


    :param [in]: parm_container_id Parm Container ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Parm group names
    """
    return _vsp.FindContainerGroupNames(parm_container_id)

@client_wrap
def FindContainerParmIDs(parm_container_id):
    r"""
    Get an array of Parm IDs included in the specified Container


    .. code-block:: python

        #==== Add Pod Geometry ====//
        pod_id = AddGeom( "POD" )

        #==== Add FeaStructure to Pod ====//
        struct_ind = AddFeaStruct( pod_id )

        #==== Get Structure Name and Parm Container ID ====//
        parm_container_name = GetFeaStructName( pod_id, struct_ind )

        parm_container_id = FindContainer( parm_container_name, struct_ind )

        #==== Get and List All Parms in the Container ====//
        parm_ids = FindContainerParmIDs( parm_container_id )

        for i in range(len(parm_ids)):

            name_id = GetParmName( parm_ids[i] ) + ": " + parm_ids[i] + "\n"

            print( name_id )


    :param [in]: parm_container_id Parm Container ID
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Parm IDs
    """
    return _vsp.FindContainerParmIDs(parm_container_id)

@client_wrap
def GetVehicleID():
    r"""
    Get the ID of the Vehicle Parm Container


    .. code-block:: python

        #===== Get Vehicle Parm Container ID ====//
        veh_id = GetVehicleID()


    :rtype: string
    :return: Vehicle ID
    """
    return _vsp.GetVehicleID()

@client_wrap
def GetNumUserParms():
    r"""
    Get the number of user parameters


    .. code-block:: python

        n = GetNumUserParms()



    :rtype: int
    :return: Number of user Parms
    """
    return _vsp.GetNumUserParms()

@client_wrap
def GetNumPredefinedUserParms():
    r"""
    Get the number of pre-defined user parameters


    .. code-block:: python

        n = GetNumPredefinedUserParms()



    :rtype: int
    :return: Number of pre-defined user Parms
    """
    return _vsp.GetNumPredefinedUserParms()

@client_wrap
def GetAllUserParms():
    r"""
    Get the vector of id's for all user parameters


    .. code-block:: python

        id_arr = GetAllUserParms()

        print( "---> User Parm IDs: " )

        for i in range(int( len(id_arr) )):

            message = "\t" + id_arr[i] + "\n"

            print( message )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of user parameter ids
    """
    return _vsp.GetAllUserParms()

@client_wrap
def GetUserParmContainer():
    r"""
    Get the user parm container ID


    .. code-block:: python

        up_id = GetUserParmContainer()


    :rtype: string
    :return: User parm container ID
    """
    return _vsp.GetUserParmContainer()

@client_wrap
def AddUserParm(type, name, group):
    r"""
    Function to add a new user Parm of input type, name, and group


    .. code-block:: python

        length = AddUserParm( PARM_DOUBLE_TYPE, "Length", "Design" )

        SetParmValLimits( length, 10.0, 0.001, 1.0e12 )

        SetParmDescript( length, "Length user parameter" )


    See also: PARM_TYPE
    :param [in]: type Parm type enum (i.e. PARM_DOUBLE_TYPE)
    :param [in]: name Parm name
    :param [in]: group Parm group
    :rtype: string
    :return: Parm ID
    """
    return _vsp.AddUserParm(type, name, group)

@client_wrap
def DeleteUserParm(id):
    r"""
    Get the user parm container ID


    .. code-block:: python


        n = GetNumPredefinedUserParms()
        id_arr = GetAllUserParms()

        if  len(id_arr) > n :
            DeleteUserParm( id_arr[n] )


    """
    return _vsp.DeleteUserParm(id)

@client_wrap
def DeleteAllUserParm():
    r"""
    Get the user parm container ID


    .. code-block:: python

        DeleteAllUserParm()


    """
    return _vsp.DeleteAllUserParm()

@client_wrap
def ComputeMinClearanceDistance(*args):
    r"""
    Compute the minimum clearance distance for the specified geometry


    .. code-block:: python

        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        pid = AddGeom( "POD", "" )                     # Add Pod

        x = GetParm( pid, "X_Rel_Location", "XForm" )

        SetParmVal( x, 3.0 )

        Update()

        min_dist = ComputeMinClearanceDistance( pid, SET_ALL )


    :param [in]: geom_id string Geom ID
    :param [in]: set Collision set enum (i.e. SET_ALL)
    :rtype: float
    :return: Minimum clearance distance
    """
    return _vsp.ComputeMinClearanceDistance(*args)

@client_wrap
def SnapParm(*args):
    r"""
    Snap the specified Parm to input target minimum clearance distance


    .. code-block:: python

        #Add Geoms
        fid = AddGeom( "FUSELAGE", "" )             # Add Fuselage

        pid = AddGeom( "POD", "" )                     # Add Pod

        x = GetParm( pid, "X_Rel_Location", "XForm" )

        SetParmVal( x, 3.0 )

        Update()

        min_dist = SnapParm( x, 0.1, True, SET_ALL )


    :param [in]: parm_id string Parm ID
    :param [in]: target_min_dist Target minimum clearance distance
    :param [in]: inc_flag Direction indication flag. If true, upper parm limit is used and direction is set to positive
    :param [in]: set Collision set enum (i.e. SET_ALL)
    :rtype: float
    :return: Minimum clearance distance
    """
    return _vsp.SnapParm(*args)

@client_wrap
def AddVarPresetGroup(group_name):
    r"""
    Add a Variable Presets group


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        if  len(GetVarPresetGroupNames()) != 1 : print( "---> Error: API AddVarPresetGroup" )


    :param [in]: group_name Variable Presets group name
    """
    return _vsp.AddVarPresetGroup(group_name)

@client_wrap
def AddVarPresetSetting(setting_name):
    r"""
    Add a setting to the currently active Variable Preset


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        if len(GetVarPresetSettingNamesWName( "Tess" )) != 1 : print( "---> Error: API AddVarPresetSetting" )


    :param [in]: setting_name Variable Presets setting name
    """
    return _vsp.AddVarPresetSetting(setting_name)

@client_wrap
def AddVarPresetParm(*args):
    r"""
    *Overload 1:*



    Add a Parm to the currently active Variable Preset


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )


    :param [in]: parm_id string Parm ID


    |

    *Overload 2:*



    Add a Parm to the currently active Variable Preset


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )


    :param [in]: parm_id string Parm ID
    :param [in]: group_name string Variable Presets group name
    """
    return _vsp.AddVarPresetParm(*args)

@client_wrap
def EditVarPresetParm(*args):
    r"""
    *Overload 1:*



    Edit the value of a Parm in the currently active Variable Preset


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        EditVarPresetParm( p1, 5 )


    :param [in]: parm_id string Parm ID
    :param [in]: parm_val double Parm value


    |

    *Overload 2:*



    Edit the value of a Parm in the currently active Variable Preset


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        EditVarPresetParm( p1, 5 )


    :param [in]: parm_id string Parm ID
    :param [in]: parm_val double Parameter value
    :param [in]: group_name string Variable Presets group name
    :param [in]: setting_name string Variable Presets setting name
    """
    return _vsp.EditVarPresetParm(*args)

@client_wrap
def DeleteVarPresetParm(*args):
    r"""
    *Overload 1:*



    Remove a Parm from the currently active Variable Preset group


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        DeleteVarPresetParm( p1 )


    :param [in]: parm_id string Parm ID


    |

    *Overload 2:*



    Remove a Parm from the currently active Variable Preset group


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        DeleteVarPresetParm( p1 )


    :param [in]: parm_id string Parm ID
    :param [in]: group_name string Variable Presets group name
    """
    return _vsp.DeleteVarPresetParm(*args)

@client_wrap
def SwitchVarPreset(group_name, setting_name):
    r"""
    Change the currently active Variable Preset


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Config" )

        AddVarPresetSetting( "Default" )

        p1 = FindParm( pod1, "Y_Rel_Rotation", "XForm" )
        p2 = FindParm( pod1, "Z_Rel_Rotation", "XForm" )

        AddVarPresetParm( p1 )
        AddVarPresetParm( p2 )

        SwitchVarPreset( "Config", "Default" )


    :param [in]: group_name Variable Presets group name
    :param [in]: setting_name Variable Presets setting name
    """
    return _vsp.SwitchVarPreset(group_name, setting_name)

@client_wrap
def DeleteVarPresetSet(group_name, setting_name):
    r"""
    Delete a Variable Preset


    .. code-block:: python

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Fine" )

        DeleteVarPresetSet( "Tess", "Fine" )

        if  len(GetVarPresetSettingNamesWName( "Tess" )) != 0 : print( "---> Error: DeleteVarPresetSet" )


    :param [in]: group_name Variable Presets group
    :param [in]: setting_name Variable Presets setting name
    :rtype: boolean
    :return: true is successful, false otherwise
    """
    return _vsp.DeleteVarPresetSet(group_name, setting_name)

@client_wrap
def GetCurrentGroupName():
    r"""
    Get the currently active Variable Presets group name


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        AddVarPresetGroup( "New_Group" )

        AddVarPresetSetting( "New_Setting" )

        print( "Current Group: " )

        print( GetCurrentGroupName() )


    :rtype: string
    :return: Variable Presets group name
    """
    return _vsp.GetCurrentGroupName()

@client_wrap
def GetCurrentSettingName():
    r"""
    Get the currently active Variable Presets setting name


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        AddVarPresetGroup( "New_Group" )

        AddVarPresetSetting( "New_Setting" )

        print( "Current Setting: " )

        print( GetCurrentSettingName() )


    :rtype: string
    :return: Variable Presets setting name
    """
    return _vsp.GetCurrentSettingName()

@client_wrap
def GetVarPresetGroupNames():
    r"""
    Get all Variable Preset group names


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        if  len(GetVarPresetGroupNames()) != 1 : print( "---> Error: API AddVarPresetGroup" )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Variable Presets group names
    """
    return _vsp.GetVarPresetGroupNames()

@client_wrap
def GetVarPresetSettingNamesWName(group_name):
    r"""
    Get the name of each settings in the specified Variable Presets group name


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        if len(GetVarPresetSettingNamesWName( "Tess" )) != 1 : print( "---> Error: API AddVarPresetSetting" )


    :param [in]: group_name Variable Presets group name
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Variable Presets setting names
    """
    return _vsp.GetVarPresetSettingNamesWName(group_name)

@client_wrap
def GetVarPresetSettingNamesWIndex(group_index):
    r"""
    Get the name of each settings in the specified Variable Presets group index


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        AddVarPresetGroup( "New_Group" )

        AddVarPresetSetting( "New_Setting_1" )
        AddVarPresetSetting( "New_Setting_2" )

        group_1_settings = GetVarPresetSettingNamesWIndex( 1 )

        if  len(group_1_settings) != 2 : print( "---> Error: API GetVarPresetSettingNamesWIndex" )


    :param [in]: group_index Variable Presets group index
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Variable Presets setting names
    """
    return _vsp.GetVarPresetSettingNamesWIndex(group_index)

@client_wrap
def GetVarPresetParmVals():
    r"""
    Get the value of each Parm in the currently active Variable Preset group and setting


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        EditVarPresetParm( p1, 5 )

        p_vals = GetVarPresetParmVals()

        if  p_vals[0] != 5 : print ( "---> Error: API EditVarPresetParm" )


    :rtype: std::vector< double,std::allocator< double > >
    :return: Array of Variable Presets Parm values
    """
    return _vsp.GetVarPresetParmVals()

@client_wrap
def GetVarPresetParmValsWNames(group_name, setting_name):
    r"""
    Get the value of each Parm in the specified Variable Preset group and setting
    param [in] group_name Variable Presets group name
    param [in] setting_name Variable Presets setting name


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "New_Group" )

        AddVarPresetSetting( "New_Setting_1" )
        AddVarPresetSetting( "New_Setting_2" )

        p1 = FindParm( pod1, "Y_Rel_Rotation", "XForm" )
        p2 = FindParm( pod1, "Z_Rel_Rotation", "XForm" )

        AddVarPresetParm( p1 )
        AddVarPresetParm( p2 )

        EditVarPresetParm( p2, 2, "New_Group", "New_Setting_2" )

        parm_vals = GetVarPresetParmValsWNames( "New_Group", "New_Setting_2" )

        if  len(parm_vals) != 2 : print( "---> Error: API GetVarPresetParmValsWNames" )


    :rtype: std::vector< double,std::allocator< double > >
    :return: Array of Variable Presets Parm values
    """
    return _vsp.GetVarPresetParmValsWNames(group_name, setting_name)

@client_wrap
def GetVarPresetParmIDs():
    r"""
    Get the Parm IDs contained in the currently active Variable Presets group


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "Tess" )

        AddVarPresetSetting( "Coarse" )

        p1 = FindParm( pod1, "Tess_U", "Shape" )

        AddVarPresetParm( p1 )

        p_IDs = GetVarPresetParmIDs()

        if  len(p_IDs) != 1 : print( "---> Error: API AddVarPresetParm" )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Variable Presets Parm IDs
    """
    return _vsp.GetVarPresetParmIDs()

@client_wrap
def GetVarPresetParmIDsWName(group_name):
    r"""
    Get the Parm IDs contained in the specitied Variable Presets group


    .. code-block:: python

        # Add Pod Geom
        pod1 = AddGeom( "POD", "" )

        AddVarPresetGroup( "New_Group" )

        AddVarPresetSetting( "New_Setting_1" )
        AddVarPresetSetting( "New_Setting_2" )

        p1 = FindParm( pod1, "Y_Rel_Rotation", "XForm" )
        p2 = FindParm( pod1, "Z_Rel_Rotation", "XForm" )

        AddVarPresetParm( p1 )
        AddVarPresetParm( p2 )

        parm_ids = GetVarPresetParmIDsWName( "New_Group" )

        if  len(parm_ids) != 2 : print( "---> Error: API GetVarPresetParmIDsWName" )


    :param [in]: group_name Variable Presets group name
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of Parm IDs
    """
    return _vsp.GetVarPresetParmIDsWName(group_name)

@client_wrap
def SetPCurve(geom_id, pcurveid, tvec, valvec, newtype):
    r"""
    Set the parameters, values, and curve type of a propeller blade curve (P Curve)
    See also: PCURV_TYPE
    :param [in]: geom_id string Parent Geom ID
    :param [in]: pcurveid P Curve index
    :param [in]: tvec Array of parameter values
    :param [in]: valvec Array of values
    :param [in]: newtype Curve type enum (i.e. CEDIT)
    """
    return _vsp.SetPCurve(geom_id, pcurveid, tvec, valvec, newtype)

@client_wrap
def PCurveConvertTo(geom_id, pcurveid, newtype):
    r"""
    Change the type of a propeller blade curve (P Curve)
    See also: PCURV_TYPE
    :param [in]: geom_id string Parent Geom ID
    :param [in]: pcurveid P Curve index
    :param [in]: newtype Curve type enum (i.e. CEDIT)
    """
    return _vsp.PCurveConvertTo(geom_id, pcurveid, newtype)

@client_wrap
def PCurveGetType(geom_id, pcurveid):
    r"""
    Get the type of a propeller blade curve (P Curve)
    See also: PCURV_TYPE
    :param [in]: geom_id string Parent Geom ID
    :param [in]: pcurveid P Curve index
    :rtype: int
    :return: Curve type enum (i.e. CEDIT)
    """
    return _vsp.PCurveGetType(geom_id, pcurveid)

@client_wrap
def PCurveGetTVec(geom_id, pcurveid):
    r"""
    Get the parameters of a propeller blade curve (P Curve). Each parameter is a fraction of propeller radius.
    :param [in]: geom_id string Parent Geom ID
    :param [in]: pcurveid P Curve index
    :rtype: std::vector< double,std::allocator< double > >
    :return: Array of parameters
    """
    return _vsp.PCurveGetTVec(geom_id, pcurveid)

@client_wrap
def PCurveGetValVec(geom_id, pcurveid):
    r"""
    Get the values of a propeller blade curve (P Curve). What the values represent id dependent on the curve type (i.e. twist, chord, etc.).
    :param [in]: geom_id string Parent Geom ID
    :param [in]: pcurveid P Curve index
    :rtype: std::vector< double,std::allocator< double > >
    :return: Array of values
    """
    return _vsp.PCurveGetValVec(geom_id, pcurveid)

@client_wrap
def PCurveDeletePt(geom_id, pcurveid, indx):
    r"""
    Delete a propeller blade curve (P Curve) point
    :param [in]: geom_id string Parent Geom ID
    :param [in]: pcurveid P Curve index
    :param [in]: indx Point index
    """
    return _vsp.PCurveDeletePt(geom_id, pcurveid, indx)

@client_wrap
def PCurveSplit(geom_id, pcurveid, tsplit):
    r"""
    Split a propeller blade curve (P Curve) at the specified 1D parameter
    :param [in]: geom_id string Parent Geom ID
    :param [in]: pcurveid P Curve index
    :param [in]: tsplit 1D parameter split location
    :rtype: int
    :return: Index of new control point
    """
    return _vsp.PCurveSplit(geom_id, pcurveid, tsplit)

@client_wrap
def ApproximateAllPropellerPCurves(geom_id):
    r"""
    Approximate all propeller blade curves with cubic Bezier curves.


    .. code-block:: python

        # Add Propeller
        prop = AddGeom( "PROP", "" )

        ApproximateAllPropellerPCurves( prop )



    :param [in]: geom_id string Geom ID
    """
    return _vsp.ApproximateAllPropellerPCurves(geom_id)

@client_wrap
def ResetPropellerThicknessCurve(geom_id):
    r"""
    Reset propeller T/C curve to match basic thickness of file-type airfoils.  Typically only used for a propeller that
    has been constructed with file-type airfoils across the blade.  The new thickness curve will be a PCHIP curve
    with t/c matching the propeller's XSecs -- unless it is a file XSec, then the Base thickness is used.


    .. code-block:: python

        # Add Propeller
        prop = AddGeom( "PROP", "" )

        ResetPropellerThicknessCurve( prop )



    :param [in]: geom_id string Geom ID
    """
    return _vsp.ResetPropellerThicknessCurve(geom_id)

@client_wrap
def AutoGroupVSPAEROControlSurfaces():
    r"""
    Creates the initial default grouping for the control surfaces.
    The initial grouping collects all surface copies of the sub-surface into a single group.
    For example if a wing is defined with an aileron and that wing is symmetrical about the
    xz plane there will be a surface copy of the master wing surface as well as a copy of
    the sub-surface. The two sub-surfaces may get deflected differently during analysis
    routines and can be identified uniquely by their full name.


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL )                      # Add Control Surface Sub-Surface

        #==== Add Vertical tail and set some parameters =====//
        vert_id = AddGeom( "WING" )

        SetGeomName( vert_id, "Vert" )

        SetParmValUpdate( vert_id, "TotalArea", "WingGeom", 10.0 )
        SetParmValUpdate( vert_id, "X_Rel_Location", "XForm", 8.5 )
        SetParmValUpdate( vert_id, "X_Rel_Rotation", "XForm", 90 )

        rudder_id = AddSubSurf( vert_id, SS_CONTROL )                      # Add Control Surface Sub-Surface

        AutoGroupVSPAEROControlSurfaces()

        Update()

        print( "COMPLETE\n" )
        control_group_settings_container_id = FindContainer( "VSPAEROSettings", 0 )   # auto grouping produces parm containers within VSPAEROSettings

        #==== Set Control Surface Group Deflection Angle ====//
        print( "\tSetting control surface group deflection angles..." )

        # subsurfaces get added to groups with "CSGQualities_[geom_name]_[control_surf_name]"
        # subsurfaces gain parm name is "Surf[surfndx]_Gain" starting from 0 to NumSymmetricCopies-1

        deflection_gain_id = FindParm( control_group_settings_container_id, "Surf_" + aileron_id + "_0_Gain", "ControlSurfaceGroup_0" )
        deflection_gain_id = FindParm( control_group_settings_container_id, "Surf_" + aileron_id + "_1_Gain", "ControlSurfaceGroup_0" )

        #  deflect aileron
        deflection_angle_id = FindParm( control_group_settings_container_id, "DeflectionAngle", "ControlSurfaceGroup_0" )


    See also: CreateVSPAEROControlSurfaceGroup
    """
    return _vsp.AutoGroupVSPAEROControlSurfaces()

@client_wrap
def CreateVSPAEROControlSurfaceGroup():
    r"""
    Add a new VSPAERO control surface group using the default naming convention. The control surface group will not contain any
    control surfaces until they are added.


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL )                      # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        num_group = GetNumControlSurfaceGroups()

        if  num_group != 1 : print( "Error: CreateVSPAEROControlSurfaceGroup" )


    See also: AddSelectedToCSGroup
    :rtype: int
    :return: Index of the new VSPAERO control surface group
    """
    return _vsp.CreateVSPAEROControlSurfaceGroup()

@client_wrap
def AddAllToVSPAEROControlSurfaceGroup(CSGroupIndex):
    r"""
    Add all available control surfaces to the control surface group at the specified index


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL )                      # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        AddAllToVSPAEROControlSurfaceGroup( group_index )


    :param [in]: CSGroupIndex Index of the control surface group
    """
    return _vsp.AddAllToVSPAEROControlSurfaceGroup(CSGroupIndex)

@client_wrap
def RemoveAllFromVSPAEROControlSurfaceGroup(CSGroupIndex):
    r"""
    Remove all used control surfaces from the control surface group at the specified index


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL )                      # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        AddAllToVSPAEROControlSurfaceGroup( group_index )

        RemoveAllFromVSPAEROControlSurfaceGroup( group_index ) # Empty control surface group


    :param [in]: CSGroupIndex Index of the control surface group
    """
    return _vsp.RemoveAllFromVSPAEROControlSurfaceGroup(CSGroupIndex)

@client_wrap
def GetActiveCSNameVec(CSGroupIndex):
    r"""
    Get the names of each active (used) control surface in the control surface group at the specified index


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL )                      # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        AddAllToVSPAEROControlSurfaceGroup( group_index )

        cs_name_vec = GetActiveCSNameVec( group_index )

        print( "Active CS in Group Index #", False )
        print( group_index )

        for i in range(int( len(cs_name_vec) )):

            print( cs_name_vec[i] )


    :param [in]: CSGroupIndex Index of the control surface group
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of active control surface names
    """
    return _vsp.GetActiveCSNameVec(CSGroupIndex)

@client_wrap
def GetCompleteCSNameVec():
    r"""
    Get the names of all control surfaces. Some may be active (used) while others may be available.


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL )                      # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        cs_name_vec = GetCompleteCSNameVec()

        print( "All Control Surfaces: ", False )

        for i in range(int( len(cs_name_vec) )):

            print( cs_name_vec[i] )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of all control surface names
    """
    return _vsp.GetCompleteCSNameVec()

@client_wrap
def GetAvailableCSNameVec(CSGroupIndex):
    r"""
    Get the names of each available (not used) control surface in the control surface group at the specified index


    .. code-block:: python

        wid = AddGeom( "WING", "" ) # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL ) # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        cs_name_vec = GetAvailableCSNameVec( group_index )

        cs_ind_vec = [1]

        AddSelectedToCSGroup( cs_ind_vec, group_index ) # Add the first available control surface to the group


    :param [in]: CSGroupIndex Index of the control surface group
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of active control surface names
    """
    return _vsp.GetAvailableCSNameVec(CSGroupIndex)

@client_wrap
def SetVSPAEROControlGroupName(name, CSGroupIndex):
    r"""
    Set the name for the control surface group at the specified index


    .. code-block:: python

        wid = AddGeom( "WING", "" ) # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL ) # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        SetVSPAEROControlGroupName( "Example_CS_Group", group_index )

        print( "CS Group name: ", False )

        print( GetVSPAEROControlGroupName( group_index ) )


    :param [in]: name Name to set for the control surface group
    :param [in]: CSGroupIndex Index of the control surface group
    """
    return _vsp.SetVSPAEROControlGroupName(name, CSGroupIndex)

@client_wrap
def GetVSPAEROControlGroupName(CSGroupIndex):
    r"""
    Get the name of the control surface group at the specified index


    .. code-block:: python

        wid = AddGeom( "WING", "" ) # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL ) # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        SetVSPAEROControlGroupName( "Example_CS_Group", group_index )

        print( "CS Group name: ", False )

        print( GetVSPAEROControlGroupName( group_index ) )


    :param [in]: CSGroupIndex Index of the control surface group
    """
    return _vsp.GetVSPAEROControlGroupName(CSGroupIndex)

@client_wrap
def AddSelectedToCSGroup(selected, CSGroupIndex):
    r"""
    Add each control surfaces in the array of control surface indexes to the control surface group at the specified index.

    Warning: The indexes in input "selected" must be matched with available control surfaces identified by GetAvailableCSNameVec.
    The "selected" input uses one- based indexing to associate available control surfaces.



    .. code-block:: python

        wid = AddGeom( "WING", "" ) # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL ) # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        cs_name_vec = GetAvailableCSNameVec( group_index )

        cs_ind_vec = [0] * len(cs_name_vec)

        for i in range(int( len(cs_name_vec) )):

            cs_ind_vec[i] = i + 1

        AddSelectedToCSGroup( cs_ind_vec, group_index ) # Add all available control surfaces to the group


    See also: GetAvailableCSNameVec
    :param [in]: selected Array of control surface indexes to add to the group. Note, the integer values are one based.
    :param [in]: CSGroupIndex Index of the control surface group
    """
    return _vsp.AddSelectedToCSGroup(selected, CSGroupIndex)

@client_wrap
def RemoveSelectedFromCSGroup(selected, CSGroupIndex):
    r"""
    Remove each control surfaces in the array of control surface indexes from the control surface group at the specified index.

    Warning: The indexes in input "selected" must be matched with active control surfaces identified by GetActiveCSNameVec. The
    "selected" input uses one-based indexing to associate available control surfaces.



    .. code-block:: python

        wid = AddGeom( "WING", "" ) # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL ) # Add Control Surface Sub-Surface

        group_index = CreateVSPAEROControlSurfaceGroup() # Empty control surface group

        cs_name_vec = GetAvailableCSNameVec( group_index )

        cs_ind_vec = [0] * len(cs_name_vec)

        for i in range(int( len(cs_name_vec) )):

            cs_ind_vec[i] = i + 1

        AddSelectedToCSGroup( cs_ind_vec, group_index ) # Add the available control surfaces to the group

        remove_cs_ind_vec = [1]

        RemoveSelectedFromCSGroup( remove_cs_ind_vec, group_index ) # Remove the first control surface


    See also: GetActiveCSNameVec
    :param [in]: selected Array of control surface indexes to remove from the group. Note, the integer values are one based.
    :param [in]: CSGroupIndex Index of the control surface group
    """
    return _vsp.RemoveSelectedFromCSGroup(selected, CSGroupIndex)

@client_wrap
def GetNumControlSurfaceGroups():
    r"""
    Get the total number of control surface groups


    .. code-block:: python

        wid = AddGeom( "WING", "" )                             # Add Wing

        aileron_id = AddSubSurf( wid, SS_CONTROL )                      # Add Control Surface Sub-Surface

        #==== Add Horizontal tail and set some parameters =====//
        horiz_id = AddGeom( "WING", "" )

        SetGeomName( horiz_id, "Vert" )

        SetParmValUpdate( horiz_id, "TotalArea", "WingGeom", 10.0 )
        SetParmValUpdate( horiz_id, "X_Rel_Location", "XForm", 8.5 )

        elevator_id = AddSubSurf( horiz_id, SS_CONTROL )                      # Add Control Surface Sub-Surface

        AutoGroupVSPAEROControlSurfaces()

        num_group = GetNumControlSurfaceGroups()

        if  num_group != 2 : print( "Error: GetNumControlSurfaceGroups" )


    :rtype: int
    :return: Number of control surface groups
    """
    return _vsp.GetNumControlSurfaceGroups()

@client_wrap
def FindActuatorDisk(disk_index):
    r"""
    Get the ID of a VSPAERO actuator disk at the specified index. An empty string is returned if
    the index is out of range.


    .. code-block:: python

        # Add a propeller
        prop_id = AddGeom( "PROP", "" )
        SetParmVal( prop_id, "PropMode", "Design", PROP_DISK )
        SetParmVal( prop_id, "Diameter", "Design", 6.0 )

        Update()

        # Setup the actuator disk VSPAERO parms
        disk_id = FindActuatorDisk( 0 )

        SetParmVal( FindParm( disk_id, "RotorRPM", "Rotor" ), 1234.0 )
        SetParmVal( FindParm( disk_id, "RotorCT", "Rotor" ), 0.35 )
        SetParmVal( FindParm( disk_id, "RotorCP", "Rotor" ), 0.55 )
        SetParmVal( FindParm( disk_id, "RotorHubDiameter", "Rotor" ), 1.0 )


    See also: PROP_MODE
    :param [in]: disk_index Actuator disk index for the current VSPAERO set
    :rtype: string
    :return: Actuator disk ID
    """
    return _vsp.FindActuatorDisk(disk_index)

@client_wrap
def GetNumActuatorDisks():
    r"""
    Get the number of actuator disks in the current VSPAERO set. This is equivalent to the number of disk surfaces in the VSPAERO set.


    .. code-block:: python

        # Set VSPAERO set index to SET_ALL
        SetParmVal( FindParm( FindContainer( "VSPAEROSettings", 0 ), "GeomSet", "VSPAERO" ), SET_ALL )

        # Add a propeller
        prop_id = AddGeom( "PROP", "" )
        SetParmValUpdate( prop_id, "PropMode", "Design", PROP_BLADES )

        num_disk = GetNumActuatorDisks() # Should be 0

        SetParmValUpdate( prop_id, "PropMode", "Design", PROP_DISK )

        num_disk = GetNumActuatorDisks() # Should be 1


    See also: PROP_MODE
    :rtype: int
    :return: Number of actuator disks in the current VSPAERO set
    """
    return _vsp.GetNumActuatorDisks()

@client_wrap
def FindUnsteadyGroup(group_index):
    r"""
    Get the ID of the VSPAERO unsteady group at the specified index. An empty string is returned if
    the index is out of range.


    .. code-block:: python

        wing_id = AddGeom( "WING" )
        pod_id = AddGeom( "POD" )

        # Create an actuator disk
        prop_id = AddGeom( "PROP", "" )
        SetParmVal( prop_id, "PropMode", "Design", PROP_BLADES )

        Update()

        # Setup the unsteady group VSPAERO parms
        disk_id = FindUnsteadyGroup( 1 ) # fixed components are in group 0 (wing & pod)

        SetParmVal( FindParm( disk_id, "RPM", "UnsteadyGroup" ), 1234.0 )


    See also: PROP_MODE
    :param [in]: group_index Unsteady group index for the current VSPAERO set
    :rtype: string
    :return: Unsteady group ID
    """
    return _vsp.FindUnsteadyGroup(group_index)

@client_wrap
def GetUnsteadyGroupName(group_index):
    r"""
    Get the name of the unsteady group at the specified index.


    .. code-block:: python

        # Add a pod and wing
        pod_id = AddGeom( "POD", "" )
        wing_id = AddGeom( "WING", pod_id )

        SetParmVal( wing_id, "X_Rel_Location", "XForm", 2.5 )
        Update()

        print( GetUnsteadyGroupName( 0 ) )


    See also: SetUnsteadyGroupName
    :param [in]: group_index Unsteady group index for the current VSPAERO set
    :rtype: string
    :return: Unsteady group name
    """
    return _vsp.GetUnsteadyGroupName(group_index)

@client_wrap
def GetUnsteadyGroupCompIDs(group_index):
    r"""
    Get an array of IDs for all components in the unsteady group at the specified index.


    .. code-block:: python

        # Add a pod and wing
        pod_id = AddGeom( "POD", "" )
        wing_id = AddGeom( "WING", pod_id ) # Default with symmetry on -> 2 surfaces

        SetParmVal( wing_id, "X_Rel_Location", "XForm", 2.5 )
        Update()

        comp_ids = GetUnsteadyGroupCompIDs( 0 )

        if  len(comp_ids) != 3 :
            print( "ERROR: GetUnsteadyGroupCompIDs" )


    See also: GetUnsteadyGroupSurfIndexes
    :param [in]: group_index Unsteady group index for the current VSPAERO set
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of component IDs
    """
    return _vsp.GetUnsteadyGroupCompIDs(group_index)

@client_wrap
def GetUnsteadyGroupSurfIndexes(group_index):
    r"""
    Get an array of surface indexes for all components in the unsteady group at the specified index.


    .. code-block:: python

        # Add a pod and wing
        pod_id = AddGeom( "POD", "" )
        wing_id = AddGeom( "WING", pod_id ) # Default with symmetry on -> 2 surfaces

        SetParmVal( wing_id, "X_Rel_Location", "XForm", 2.5 )
        Update()

        surf_indexes = GetUnsteadyGroupSurfIndexes( 0 )

        if  len(surf_indexes) != 3 :
            print( "ERROR: GetUnsteadyGroupSurfIndexes" )


    See also: GetUnsteadyGroupCompIDs
    :param [in]: group_index Unsteady group index for the current VSPAERO set
    :rtype: std::vector< int,std::allocator< int > >
    :return: Array of surface indexes
    """
    return _vsp.GetUnsteadyGroupSurfIndexes(group_index)

@client_wrap
def GetNumUnsteadyGroups():
    r"""
    Get the number of unsteady groups in the current VSPAERO set. Each propeller is placed in its own unsteady group. All symmetric copies
    of propellers are also placed in an unsteady group. All other component types are placed in a single fixed component unsteady group.


    .. code-block:: python

        # Set VSPAERO set index to SET_ALL
        SetParmVal( FindParm( FindContainer( "VSPAEROSettings", 0 ), "GeomSet", "VSPAERO" ), SET_ALL )

        # Add a propeller
        prop_id = AddGeom( "PROP" )
        SetParmValUpdate( prop_id, "PropMode", "Design", PROP_DISK )

        num_group = GetNumUnsteadyGroups() # Should be 0

        SetParmValUpdate( prop_id, "PropMode", "Design", PROP_BLADES )

        num_group = GetNumUnsteadyGroups() # Should be 1

        wing_id = AddGeom( "WING" )

        num_group = GetNumUnsteadyGroups() # Should be 2 (includes fixed component group)


    See also: PROP_MODE, GetNumUnsteadyRotorGroups
    :rtype: int
    :return: Number of unsteady groups in the current VSPAERO set
    """
    return _vsp.GetNumUnsteadyGroups()

@client_wrap
def GetNumUnsteadyRotorGroups():
    r"""
    Get the number of unsteady rotor groups in the current VSPAERO set. This is equivalent to the total number of propeller Geoms,
    including each symmetric copy, in the current VSPAERO set. While all fixed components (wings, fuseleage, etc.) are placed in
    their own unsteady group, this function does not consider them.


    .. code-block:: python

        # Set VSPAERO set index to SET_ALL
        SetParmVal( FindParm( FindContainer( "VSPAEROSettings", 0 ), "GeomSet", "VSPAERO" ), SET_ALL )

        # Add a propeller
        prop_id = AddGeom( "PROP" )
        SetParmValUpdate( prop_id, "PropMode", "Design", PROP_DISK )

        num_group = GetNumUnsteadyRotorGroups() # Should be 0

        SetParmValUpdate( prop_id, "PropMode", "Design", PROP_BLADES )

        num_group = GetNumUnsteadyRotorGroups() # Should be 1

        wing_id = AddGeom( "WING" )

        num_group = GetNumUnsteadyRotorGroups() # Should be 1 still (fixed group not included)


    See also: PROP_MODE, GetNumUnsteadyGroups
    :rtype: int
    :return: Number of unsteady rotor groups in the current VSPAERO set
    """
    return _vsp.GetNumUnsteadyRotorGroups()

@client_wrap
def AddExcrescence(excresName, excresType, excresVal):
    r"""
    Add an Excresence to the Parasite Drag Tool


    .. code-block:: python

        AddExcrescence( "Miscellaneous", EXCRESCENCE_COUNT, 8.5 )

        AddExcrescence( "Cowl Boattail", EXCRESCENCE_CD, 0.0003 )


    See also: EXCRES_TYPE
    :param [in]: excresName Name of the Excressence
    :param [in]: excresType Excressence type enum (i.e. EXCRESCENCE_PERCENT_GEOM)
    :param [in]: excresVal Excressence value
    """
    return _vsp.AddExcrescence(excresName, excresType, excresVal)

@client_wrap
def DeleteExcrescence(index):
    r"""
    Delete an Excresence from the Parasite Drag Tool


    .. code-block:: python

        AddExcrescence( "Miscellaneous", EXCRESCENCE_COUNT, 8.5 )

        AddExcrescence( "Cowl Boattail", EXCRESCENCE_CD, 0.0003 )

        AddExcrescence( "Percentage Example", EXCRESCENCE_PERCENT_GEOM, 5 )

        DeleteExcrescence( 2 ) # Last Index


    :param [in]: index int Index of the Excressence to delete
    """
    return _vsp.DeleteExcrescence(index)

@client_wrap
def UpdateParasiteDrag():
    r"""    Update any reference geometry, atmospheric properties, excressences, etc. in the Parasite Drag Tool"""
    return _vsp.UpdateParasiteDrag()

@client_wrap
def WriteAtmosphereCSVFile(file_name, atmos_type):
    r"""
    Calculate the atmospheric properties determined by a specified model for a preset array of altitudes ranging from 0 to 90000 m and
    write the results to a CSV output file


    .. code-block:: python

        print( "Starting USAF Atmosphere 1966 Table Creation. \n" )

        WriteAtmosphereCSVFile( "USAFAtmosphere1966Data.csv", ATMOS_TYPE_HERRINGTON_1966 )


    See also: ATMOS_TYPE
    :param [in]: file_name Output CSV file
    :param [in]: atmos_type Atmospheric model enum (i.e. ATMOS_TYPE_HERRINGTON_1966)
    """
    return _vsp.WriteAtmosphereCSVFile(file_name, atmos_type)

@client_wrap
def CalcAtmosphere(alt, delta_temp, atmos_type):
    r"""
    Calculate the atmospheric properties determined by a specified model at input altitude and temperature deviation. This function may
    not be used for any manual atmospheric model types (i.e. ATMOS_TYPE_MANUAL_P_T). This function assumes freestream units are metric,
    temperature units are Kelvin, and pressure units are kPA.


    .. code-block:: python


        alt = 4000

        delta_temp = 0

        temp, pres, pres_ratio, rho_ratio = CalcAtmosphere( alt, delta_temp, ATMOS_TYPE_US_STANDARD_1976)


    See also: ATMOS_TYPE
    :param [in]: alt Altitude
    :param [in]: delta_temp Deviation in temperature from the value specified in the atmospheric model
    :param [in]: atmos_type Atmospheric model enum (i.e. ATMOS_TYPE_HERRINGTON_1966)
    :param [out]: temp output Temperature
    :param [out]: pres output Pressure
    :param [out]: pres_ratio Output pressure ratio
    :param [out]: rho_ratio Output density ratio
    """
    return _vsp.CalcAtmosphere(alt, delta_temp, atmos_type)

@client_wrap
def WriteBodyFFCSVFile(file_name):
    r"""
    Calculate the form factor from each body FF equation (i.e. Hoerner Streamlined Body) and write the results to a CSV output file


    .. code-block:: python

        print( "Starting Body Form Factor Data Creation. \n" )
        WriteBodyFFCSVFile( "BodyFormFactorData.csv" )


    :param [in]: file_name Output CSV file
    """
    return _vsp.WriteBodyFFCSVFile(file_name)

@client_wrap
def WriteWingFFCSVFile(file_name):
    r"""
    Calculate the form factor from each wing FF equation (i.e. Schemensky 4 Series Airfoil) and write the results to a CSV output file


    .. code-block:: python

        print( "Starting Wing Form Factor Data Creation. \n" )
        WriteWingFFCSVFile( "WingFormFactorData.csv" )


    :param [in]: file_name Output CSV file
    """
    return _vsp.WriteWingFFCSVFile(file_name)

@client_wrap
def WriteCfEqnCSVFile(file_name):
    r"""
    Calculate the coefficient of friction from each Cf equation (i.e. Power Law Blasius) and write the results to a CSV output file


    .. code-block:: python

        print( "Starting Turbulent Friciton Coefficient Data Creation. \n" )
        WriteCfEqnCSVFile( "FrictionCoefficientData.csv" )


    :param [in]: file_name Output CSV file
    """
    return _vsp.WriteCfEqnCSVFile(file_name)

@client_wrap
def WritePartialCfMethodCSVFile(file_name):
    r"""
    Calculate the partial coefficient of friction and write the results to a CSV output file


    .. code-block:: python

        print( "Starting Partial Friction Method Data Creation. \n" )
        WritePartialCfMethodCSVFile( "PartialFrictionMethodData.csv" )


    :param [in]: file_name Output CSV file
    """
    return _vsp.WritePartialCfMethodCSVFile(file_name)

@client_wrap
def CompPnt01(geom_id, surf_indx, u, w):
    r"""
    Calculate the 3D coordinate equivalent for the input surface coordinate point


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        pnt = CompPnt01( geom_id, surf_indx, u, w )

        print( f"Point: ( {pnt.x()}, {pnt.y()}, {pnt.z()} )" )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: u U (0 - 1) surface coordinate
    :param [in]: w W (0 - 1) surface coordinate
    :rtype: :py:class:`vec3d`
    :return: Normal vector3D coordinate point
    """
    return _vsp.CompPnt01(geom_id, surf_indx, u, w)

@client_wrap
def CompNorm01(geom_id, surf_indx, u, w):
    r"""
    Calculate the normal vector on the specified surface at input surface coordinate


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        norm = CompNorm01( geom_id, surf_indx, u, w )

        print( "Point: ( {norm.x()}, {norm.y()}, {norm.z()} )" )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: u U (0 - 1) surface coordinate
    :param [in]: w W (0 - 1) surface coordinate
    :rtype: :py:class:`vec3d`
    :return: Normal vector
    """
    return _vsp.CompNorm01(geom_id, surf_indx, u, w)

@client_wrap
def CompTanU01(geom_id, surf_indx, u, w):
    r"""
    Calculate the vector tangent to the specified surface at input surface coordinate in the U direction


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        tanu = CompTanU01( geom_id, surf_indx, u, w )

        print( f"Point: ( {tanu.x()}, {tanu.y()}, {tanu.z()} )" )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: u U (0 - 1) surface coordinate
    :param [in]: w W (0 - 1) surface coordinate
    :rtype: :py:class:`vec3d`
    :return: Tangent vector in U direction
    """
    return _vsp.CompTanU01(geom_id, surf_indx, u, w)

@client_wrap
def CompTanW01(geom_id, surf_indx, u, w):
    r"""
    Calculate the vector tangent to the specified surface at input surface coordinate in the W direction


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        tanw = CompTanW01( geom_id, surf_indx, u, w )

        print( f"Point: ( {tanw.x()}, {tanw.y()}, {tanw.z()} )" )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: u U (0 - 1) surface coordinate
    :param [in]: w W (0 - 1) surface coordinate
    :rtype: :py:class:`vec3d`
    :return: Tangent vector in W direction
    """
    return _vsp.CompTanW01(geom_id, surf_indx, u, w)

@client_wrap
def CompCurvature01(geom_id, surf_indx, u, w):
    r"""
    Determine the curvature of a specified surface at the input surface coordinate point


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0


        u = 0.25
        w = 0.75

        k1, k2, ka, kg = CompCurvature01( geom_id, surf_indx, u, w )

        print( f"Curvature : k1 {k1} k2 {k2} ka {ka} kg {kg}" )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: u double U (0 - 1) surface coordinate
    :param [in]: w double W (0 - 1) surface coordinate
    :param [out]: k1_out double Output value of maximum principal curvature
    :param [out]: k2_out double Output value of minimum principal curvature
    :param [out]: ka_out double Output value of mean curvature
    :param [out]: kg_out double Output value of Gaussian curvature
    """
    return _vsp.CompCurvature01(geom_id, surf_indx, u, w)

@client_wrap
def ProjPnt01(geom_id, surf_indx, pt):
    r"""
    Determine the nearest surface coordinate for an input 3D coordinate point and calculate the distance between the
    3D point and the closest point of the surface.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        pnt = CompPnt01( geom_id, surf_indx, u, w )

        norm = CompNorm01( geom_id, surf_indx, u, w )


        # Offset point from surface
        pnt.set_xyz( pnt.x() + norm.x(), pnt.y() + norm.y(), pnt.z() + norm.z() )

        d, uout, wout = ProjPnt01( geom_id, surf_indx, pnt )

        print( f"Dist {d} u {uout} w {wout}" )


    See also: ProjPnt01Guess, ProjPnt01I
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pt vec3d Input 3D coordinate point
    :param [out]: u_out double Output closest U (0 - 1) surface coordinate
    :param [out]: w_out double Output closest W (0 - 1) surface coordinate
    :rtype: float
    :return: double Distance between the 3D point and the closest point of the surface
    """
    return _vsp.ProjPnt01(geom_id, surf_indx, pt)

@client_wrap
def ProjPnt01I(geom_id, pt):
    r"""
    Determine the nearest surface coordinate and corresponding parent Geom main surface index for an input 3D coordinate point. Return the distance between
    the closest point and the input.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        d = 0

        pnt = CompPnt01( geom_id, surf_indx, u, w )

        norm = CompNorm01( geom_id, surf_indx, u, w )



        # Offset point from surface
        pnt.set_xyz( pnt.x() + norm.x(), pnt.y() + norm.y(), pnt.z() + norm.z() )

        d, surf_indx_out, uout, wout = ProjPnt01I( geom_id, pnt )

        print( f"Dist {d} u {uout} w {wout} surf_index {surf_indx_out}" )


    See also: ProjPnt01, ProjPnt01Guess
    :param [in]: geom_id string Parent Geom ID
    :param [in]: pt vec3d Input 3D coordinate point
    :param [out]: surf_indx_out int Output main surface index from the parent Geom
    :param [out]: u_out double Output closest U (0 - 1) surface coordinat
    :param [out]: w_out double Output closest W (0 - 1) surface coordinat
    :rtype: float
    :return: double Distance between the 3D point and the closest point of the surface
    """
    return _vsp.ProjPnt01I(geom_id, pt)

@client_wrap
def ProjPnt01Guess(geom_id, surf_indx, pt, u0, w0):
    r"""
    Determine the nearest surface coordinate for an input 3D coordinate point and calculate the distance between the
    3D point and the closest point of the surface. This function takes an input surface coordinate guess for, offering
    a potential decrease in computation time compared to ProjPnt01.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        d = 0

        pnt = CompPnt01( geom_id, surf_indx, u, w )

        norm = CompNorm01( geom_id, surf_indx, u, w )


        # Offset point from surface
        pnt.set_xyz( pnt.x() + norm.x(), pnt.y() + norm.y(), pnt.z() + norm.z() )

        d, uout, wout = ProjPnt01Guess( geom_id, surf_indx, pnt, u + 0.1, w + 0.1 )

        print( f"Dist {d} u {uout} w {wout}" )


    See also: ProjPnt01, ProjPnt01I
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pt vec3d Input 3D coordinate point
    :param [in]: u0 double Input U (0 - 1) surface coordinate guess
    :param [in]: w0 double Input W (0 - 1) surface coordinate guess
    :param [out]: u_out double Output closest U (0 - 1) surface coordinate
    :param [out]: w_out double Output closest W (0 - 1) surface coordinate
    :rtype: float
    :return: double Distance between the 3D point and the closest point of the surface
    """
    return _vsp.ProjPnt01Guess(geom_id, surf_indx, pt, u0, w0)

@client_wrap
def AxisProjPnt01(geom_id, surf_indx, iaxis, pt):
    r"""
    Project an input 3D coordinate point onto a surface along a specified axis.  If the axis-aligned ray from the point intersects the surface multiple times, the nearest intersection is returned.  If the axis-aligned ray from the point does not intersect the surface, the original point is returned and -1 is returned in the other output parameters.



    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        surf_pt = CompPnt01( geom_id, surf_indx, u, w )
        pt = surf_pt

        pt.offset_y( -5.0 )

        idist, u_out, w_out = AxisProjPnt01( geom_id, surf_indx, Y_DIR, pt )

        print( f"iDist {idist} u_out {u_out} w_out {w_out}" )
        print( "3D Offset ", False)


    See also: AxisProjPnt01Guess, AxisProjPnt01I, AxisProjVecPnt01, AxisProjVecPnt01Guess
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: iaxis int Axis direction to project point along (X_DIR, Y_DIR, or Z_DIR)
    :param [in]: pt Input 3D coordinate point
    :param [out]: u_out Output closest U (0 - 1) surface coordinate
    :param [out]: w_out Output closest W (0 - 1) surface coordinate
    :rtype: float
    :return: Axis aligned distance between the 3D point and the projected point on the surface
    """
    return _vsp.AxisProjPnt01(geom_id, surf_indx, iaxis, pt)

@client_wrap
def AxisProjPnt01I(geom_id, iaxis, pt):
    r"""
    Project an input 3D coordinate point onto a Geom along a specified axis.  The intersecting surface index is also returned.  If the axis-aligned ray from the point intersects the Geom multiple times, the nearest intersection is returned.  If the axis-aligned ray from the point does not intersect the Geom, the original point is returned and -1 is returned in the other output parameters.



    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890

        surf_pt = CompPnt01( geom_id, surf_indx, u, w )
        pt = surf_pt

        pt.offset_y( -5.0 )


        idist, surf_indx_out, u_out, w_out = AxisProjPnt01I( geom_id, Y_DIR, pt )

        print( "iDist {idist} u_out {u_out} w_out {w_out} surf_index {surf_indx_out}" )
        print( "3D Offset ", False)


    See also: AxisProjPnt01, AxisProjPnt01Guess, AxisProjVecPnt01, AxisProjVecPnt01Guess
    :param [in]: geom_id string Parent Geom ID
    :param [in]: iaxis int Axis direction to project point along (X_DIR, Y_DIR, or Z_DIR)
    :param [in]: pt Input 3D coordinate point
    :param [out]: surf_indx_out Output main surface index from the parent Geom
    :param [out]: u_out Output closest U (0 - 1) surface coordinate
    :param [out]: w_out Output closest W (0 - 1) surface coordinate
    :rtype: float
    :return: Axis aligned distance between the 3D point and the projected point on the surface
    """
    return _vsp.AxisProjPnt01I(geom_id, iaxis, pt)

@client_wrap
def AxisProjPnt01Guess(geom_id, surf_indx, iaxis, pt, u0, w0):
    r"""
    Project an input 3D coordinate point onto a surface along a specified axis given an initial guess of surface parameter.  If the axis-aligned ray from the point intersects the surface multiple times, the nearest intersection is returned.  If the axis-aligned ray from the point does not intersect the surface, the original point is returned and -1 is returned in the other output parameters.  The surface parameter guess should allow this call to be faster than calling AxisProjPnt01 without a guess.



    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        u = 0.12345
        w = 0.67890



        surf_pt = CompPnt01( geom_id, surf_indx, u, w )
        pt = surf_pt

        pt.offset_y( -5.0 )

        # Construct initial guesses near actual parameters
        u0 = u + 0.01234
        w0 = w - 0.05678

        d, uout, wout = AxisProjPnt01Guess( geom_id, surf_indx, Y_DIR, pt, u0, w0 )

        print( f"Dist {d} u {uout} w {wout}" )


    See also: AxisProjPnt01, AxisProjPnt01I, AxisProjVecPnt01, AxisProjVecPnt01Guess
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: iaxis int Axis direction to project point along (X_DIR, Y_DIR, or Z_DIR)
    :param [in]: pt Input 3D coordinate point
    :param [in]: u0 Input U (0 - 1) surface coordinate guess
    :param [in]: w0 Input W (0 - 1) surface coordinate guess
    :param [out]: u_out Output closest U (0 - 1) surface coordinate
    :param [out]: w_out Output closest W (0 - 1) surface coordinate
    :rtype: float
    :return: Distance between the 3D point and the closest point of the surface
    """
    return _vsp.AxisProjPnt01Guess(geom_id, surf_indx, iaxis, pt, u0, w0)

@client_wrap
def InsideSurf(geom_id, surf_indx, pt):
    r"""
    Test whether a given point is inside a specified surface.



    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        r = 0.12
        s = 0.68
        t = 0.56

        pnt = CompPntRST( geom_id, surf_indx, r, s, t )

        res = InsideSurf( geom_id, surf_indx, pnt )

        if  res :
            print( "Inside" )
        else:
            print( "Outside" )



    See also: VecInsideSurf
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pt Input 3D coordinate point
    :rtype: boolean
    :return: Boolean true if the point is inside the surface, false otherwise.
    """
    return _vsp.InsideSurf(geom_id, surf_indx, pt)

@client_wrap
def CompPntRST(geom_id, surf_indx, r, s, t):
    r"""
    Calculate the (X, Y, Z) coordinate for the input volume (R, S, T) coordinate point


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        r = 0.12
        s = 0.68
        t = 0.56

        pnt = CompPntRST( geom_id, surf_indx, r, s, t )

        print( f"Point: ( {pnt.x()}, {pnt.y()}, {pnt.z()} )" )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: r R (0 - 1) volume coordinate
    :param [in]: s S (0 - 1) volume coordinate
    :param [in]: t T (0 - 1) volume coordinate
    :rtype: :py:class:`vec3d`
    :return: vec3d coordinate point
    """
    return _vsp.CompPntRST(geom_id, surf_indx, r, s, t)

@client_wrap
def FindRST(geom_id, surf_indx, pt):
    r"""
    Determine the nearest (R, S, T) volume coordinate for an input (X, Y, Z) 3D coordinate point and calculate the distance between the
    3D point and the found volume point.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        r = 0.12
        s = 0.68
        t = 0.56

        pnt = CompPntRST( geom_id, surf_indx, r, s, t )


        d, rout, sout, tout = FindRST( geom_id, surf_indx, pnt )

        print( f"Dist {d} r {rout} s {sout} t {tout}" )


    See also: FindRSTGuess
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pt vec3d Input 3D coordinate point
    :param [out]: r_out double Output closest R (0 - 1.0) volume coordinate
    :param [out]: s_out double Output closest S (0 - 1.0) volume coordinate
    :param [out]: t_out double Output closest T (0 - 1.0) volume coordinate
    :rtype: float
    :return: double Distance between the 3D point and the closest point of the volume
    """
    return _vsp.FindRST(geom_id, surf_indx, pt)

@client_wrap
def FindRSTGuess(geom_id, surf_indx, pt, r0, s0, t0):
    r"""
    Determine the nearest (R, S, T) volume coordinate for an input (X, Y, Z) 3D coordinate point given an initial guess of volume coordinates.  Also calculate the distance between the
    3D point and the found volume point.



    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        r = 0.12
        s = 0.68
        t = 0.56

        pnt = CompPntRST( geom_id, surf_indx, r, s, t )


        r0 = 0.1
        s0 = 0.6
        t0 = 0.5

        d, rout, sout, tout = FindRSTGuess( geom_id, surf_indx, pnt, r0, s0, t0 )

        print( f"Dist {d} r {rout} s {sout} t {tout}" )


    See also: FindRST
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pt vec3d Input 3D coordinate point
    :param [in]: r0 double Input R (0 - 1.0) volume coordinate guess
    :param [in]: s0 double Input S (0 - 1.0) volume coordinate guess
    :param [in]: t0 double Input T (0 - 1.0) volume coordinate guess
    :param [out]: r_out double Output closest R (0 - 1.0) volume coordinate
    :param [out]: s_out double Output closest S (0 - 1.0) volume coordinate
    :param [out]: t_out double Output closest T (0 - 1.0) volume coordinate
    :rtype: float
    :return: double Distance between the 3D point and the closest point of the volume
    """
    return _vsp.FindRSTGuess(geom_id, surf_indx, pt, r0, s0, t0)

@client_wrap
def ConvertRSTtoLMN(geom_id, surf_indx, r, s, t):
    r"""
    Convert RST volumetric coordinates to LMN coordinates.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        r = 0.12
        s = 0.68
        t = 0.56

        l_out, m_out, n_out = ConvertRSTtoLMN( geom_id, surf_indx, r, s, t )



    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: r R (0 - 1) volume coordinate
    :param [in]: s S (0 - 1) volume coordinate
    :param [in]: t T (0 - 1) volume coordinate
    :param [out]: l_out L (0 - 1) linear volume coordinate
    :param [out]: m_out M (0 - 1) linear volume coordinate
    :param [out]: n_out N (0 - 1) linear volume coordinate
    """
    return _vsp.ConvertRSTtoLMN(geom_id, surf_indx, r, s, t)

@client_wrap
def ConvertRtoL(geom_id, surf_indx, r):
    r"""
    Convert R volumetric coordinate to L coordinate.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        r = 0.12

        l_out = ConvertRtoL( geom_id, surf_indx, r )



    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: r R (0 - 1) volume coordinate
    :param [out]: l_out L (0 - 1) linear volume coordinate
    """
    return _vsp.ConvertRtoL(geom_id, surf_indx, r)

@client_wrap
def ConvertLMNtoRST(geom_id, surf_indx, l, m, n):
    r"""
    Convert LMN volumetric coordinates to RST coordinates.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        l = 0.12
        m = 0.34
        n = 0.56

        r_out, s_out, t_out = ConvertLMNtoRST( geom_id, surf_indx, l, m, n )



    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: l L (0 - 1) linear volume coordinate
    :param [in]: m M (0 - 1) linear volume coordinate
    :param [in]: n N (0 - 1) linear volume coordinate
    :param [out]: r_out R (0 - 1) volume coordinate
    :param [out]: s_out S (0 - 1) volume coordinate
    :param [out]: t_out T (0 - 1) volume coordinate
    """
    return _vsp.ConvertLMNtoRST(geom_id, surf_indx, l, m, n)

@client_wrap
def ConvertLtoR(geom_id, surf_indx, l):
    r"""
    Convert L volumetric coordinate to R coordinate.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        l = 0.12

        r_out = ConvertLtoR( geom_id, surf_indx, l )



    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: l L (0 - 1) volume coordinate
    :param [out]: r_out R (0 - 1) linear volume coordinate
    """
    return _vsp.ConvertLtoR(geom_id, surf_indx, l)

@client_wrap
def ConvertUtoEta(geom_id, u):
    r"""
    Convert U coordinate to eta wing coordinate.


    .. code-block:: python

        # Add Wing Geom
        geom_id = AddGeom( "WING", "" )

        surf_indx = 0

        u = 0.25

        eta_out = ConvertUtoEta( geom_id, u )



    :param [in]: geom_id string Parent Geom ID
    :param [in]: u U (0 - 1) surface coordinate
    :param [out]: eta_out Eta (0 - 1) wing spanwise coordinate
    """
    return _vsp.ConvertUtoEta(geom_id, u)

@client_wrap
def ConvertEtatoU(geom_id, eta):
    r"""
    Convert eta wing coordinate to u coordinate.


    .. code-block:: python

        # Add Wing Geom
        geom_id = AddGeom( "WING", "" )

        surf_indx = 0

        eta= 0.25

        u = ConvertEtatoU( geom_id, eta )



    :param [in]: geom_id string Parent Geom ID
    :param [in]: eta Eta (0 - 1) wing spanwise coordinate
    :param [out]: u_out U (0 - 1) surface coordinate
    """
    return _vsp.ConvertEtatoU(geom_id, eta)

@client_wrap
def CompVecPnt01(geom_id, surf_indx, u_in_vec, w_in_vec):
    r"""
    Determine 3D coordinate for each surface coordinate point in the input arrays


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        uvec = [0]*n
        wvec = [0]*n

        for i in range(n):

            uvec[i] = (i+1)*1.0/(n+1)

            wvec[i] = (n-i)*1.0/(n+1)

        ptvec = CompVecPnt01( geom_id, 0, uvec, wvec )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: u_in_vec vector<double> Input vector of U (0 - 1) surface coordinates
    :param [in]: w_in_vec vector<double> Input vector of W (0 - 1) surface coordinates
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> Vector of 3D coordinate points
    """
    return _vsp.CompVecPnt01(geom_id, surf_indx, u_in_vec, w_in_vec)

@client_wrap
def CompVecNorm01(geom_id, surf_indx, us, ws):
    r"""
    Determine the normal vector on a surface for each surface coordinate point in the input arrays


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        uvec = [0]*n
        wvec = [0]*n

        for i in range(n):

            uvec[i] = (i+1)*1.0/(n+1)

            wvec[i] = (n-i)*1.0/(n+1)

        normvec = CompVecNorm01( geom_id, 0, uvec, wvec )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: us vector<double> Input vector of U (0 - 1) surface coordinates
    :param [in]: ws vector<double> Input vector of W (0 - 1) surface coordinates
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> Vector of 3D normal vectors
    """
    return _vsp.CompVecNorm01(geom_id, surf_indx, us, ws)

@client_wrap
def CompVecCurvature01(geom_id, surf_indx, us, ws):
    r"""
    Determine the curvature of a specified surface at each surface coordinate point in the input arrays


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        uvec = [0]*n
        wvec = [0]*n

        for i in range(n):

            uvec[i] = (i+1)*1.0/(n+1)

            wvec[i] = (n-i)*1.0/(n+1)



        k1vec, k2vec, kavec, kgvec = CompVecCurvature01( geom_id, 0, uvec, wvec )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: us vector<double> Input vector of U (0 - 1) surface coordinates
    :param [in]: ws vector<double> Input vector of W (0 - 1) surface coordinates
    :param [out]: k1_out_vec vector<double> Output vector of maximum principal curvatures
    :param [out]: k2_out_vec vector<double> Output vector of minimum principal curvatures
    :param [out]: ka_out_vec vector<double> Output vector of mean curvatures
    :param [out]: kg_out_vec vector<double> Output vector of Gaussian curvatures
    """
    return _vsp.CompVecCurvature01(geom_id, surf_indx, us, ws)

@client_wrap
def ProjVecPnt01(geom_id, surf_indx, pts):
    r"""
    Determine the nearest surface coordinates for an input array of 3D coordinate points and calculate the distance between each
    3D point and the closest point of the surface.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        uvec = [0]*n
        wvec = [0]*n

        for i in range(n):

            uvec[i] = (i+1)*1.0/(n+1)

            wvec[i] = (n-i)*1.0/(n+1)

        ptvec = CompVecPnt01( geom_id, 0, uvec, wvec )

        normvec = CompVecNorm01( geom_id, 0, uvec, wvec )

        for i in range(n):

            ptvec[i].set_xyz( ptvec[i].x() + normvec[i].x(), ptvec[i].y() + normvec[i].y(), ptvec[i].z() + normvec[i].z() )

        uoutv, woutv, doutv = ProjVecPnt01( geom_id, 0, ptvec )


    See also: ProjVecPnt01Guess
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pts vector<vec3d> Input vector of 3D coordinate points
    :param [out]: u_out_vec vector<double> Output vector of the closest U (0 - 1) surface coordinate for each 3D input point
    :param [out]: w_out_vec vector<double> Output vector of the closest W (0 - 1) surface coordinate for each 3D input point
    :param [out]: d_out_vec vector<double> Output vector of distances for each 3D point and the closest point of the surface
    """
    return _vsp.ProjVecPnt01(geom_id, surf_indx, pts)

@client_wrap
def ProjVecPnt01Guess(geom_id, surf_indx, pts, u0s, w0s):
    r"""
    Determine the nearest surface coordinates for an input array of 3D coordinate points and calculate the distance between each
    3D point and the closest point of the surface. This function takes an input array of surface coordinate guesses for each 3D
    coordinate, offering a potential decrease in computation time compared to ProjVecPnt01.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        uvec = [0]*n
        wvec = [0]*n

        for i in range(n):

            uvec[i] = (i+1)*1.0/(n+1)

            wvec[i] = (n-i)*1.0/(n+1)

        ptvec = CompVecPnt01( geom_id, 0, uvec, wvec )

        normvec = CompVecNorm01( geom_id, 0, uvec, wvec )

        for i in range(n):

            ptvec[i].set_xyz( ptvec[i].x() + normvec[i].x(), ptvec[i].y() + normvec[i].y(), ptvec[i].z() + normvec[i].z() )

        u0v = [0]*n
        w0v = [0]*n

        for i in range(n):

            u0v[i] = uvec[i] + 0.01234

            w0v[i] = wvec[i] - 0.05678

        uoutv, woutv, doutv = ProjVecPnt01Guess( geom_id, 0, ptvec, u0v,  w0v )


    See also: ProjVecPnt01,
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pts vector<vec3d> Input vector of 3D coordinate points
    :param [in]: u0s vector<double> Input vector of U (0 - 1) surface coordinate guesses
    :param [in]: w0s vector<double> Input vector of W (0 - 1) surface coordinate guesses
    :param [out]: u_out_vec vector<double> Output vector of the closest U (0 - 1) surface coordinate for each 3D input point
    :param [out]: w_out_vec vector<double> Output vector of the closest W (0 - 1) surface coordinate for each 3D input point
    :param [out]: d_out_vec vector<double> Output array of distances for each 3D point and the closest point of the surface
    """
    return _vsp.ProjVecPnt01Guess(geom_id, surf_indx, pts, u0s, w0s)

@client_wrap
def AxisProjVecPnt01(geom_id, surf_indx, iaxis, pts):
    r"""
    Project an input array of 3D coordinate points onto a surface along a specified axis.  If the axis-aligned ray from the point intersects the surface multiple times, the nearest intersection is returned.  If the axis-aligned ray from the point does not intersect the surface, the original point is returned and -1 is returned in the other output parameters.




    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )
        surf_indx = 0

        n = 5

        uvec = [0]*n
        wvec = [0]*n

        for i in range(n):

            uvec[i] = (i+1)*1.0/(n+1)

            wvec[i] = (n-i)*1.0/(n+1)

        ptvec = CompVecPnt01( geom_id, surf_indx, uvec, wvec )

        for i in range(n):

            ptvec[i].offset_y( -5.0 )

        uoutv, woutv, doutv = AxisProjVecPnt01( geom_id, surf_indx, Y_DIR, ptvec )

        # Some of these outputs are expected to be non-zero because the projected point is on the opposite side of
        # the pod from the originally computed point.  I.e. there were multiple solutions and the original point
        # is not the closest intersection point.  We could offset those points in the +Y direction instead of -Y.
        for i in range(n):

            print( i, False )
            print( "U delta ", False )
            print( uvec[i] - uoutv[i], False )
            print( "W delta ", False )
            print( wvec[i] - woutv[i] )



    See also: AxisProjPnt01, AxisProjPnt01Guess, AxisProjPnt01I, AxisProjVecPnt01Guess
    :param [in]: geom_id string Geom ID
    :param [in]: surf_indx int Main surface index from the Geom
    :param [in]: iaxis int Axis direction to project point along (X_DIR, Y_DIR, or Z_DIR)
    :param [in]: pts vector<vec3d> Input vector of 3D coordinate points
    :param [out]: u_out_vec vector<double> Output vector of the closest U (0 - 1) surface coordinate for each 3D input point
    :param [out]: w_out_vec vector<double> Output vector of the closest W (0 - 1) surface coordinate for each 3D input point
    :param [out]: d_out_vec vector<double> Output vector of axis distances for each 3D point and the projected point of the surface
    """
    return _vsp.AxisProjVecPnt01(geom_id, surf_indx, iaxis, pts)

@client_wrap
def AxisProjVecPnt01Guess(geom_id, surf_indx, iaxis, pts, u0s, w0s):
    r"""
    Project an input array of 3D coordinate points onto a surface along a specified axis given initial guess arrays of surface parameter.  If the axis-aligned ray from the point intersects the surface multiple times, the nearest intersection is returned.  If the axis-aligned ray from the point does not intersect the surface, the original point is returned and -1 is returned in the other output parameters.  The surface parameter guess should allow this call to be faster than calling AxisProjVecPnt01 without a guess.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )
        surf_indx = 0

        n = 5

        uvec = [0]*n
        wvec = [0]*n

        for i in range(n):

            uvec[i] = (i+1)*1.0/(n+1)

            wvec[i] = (n-i)*1.0/(n+1)

        ptvec = CompVecPnt01( geom_id, surf_indx, uvec, wvec )

        for i in range(n):

            ptvec[i].offset_y( -5.0 )

        u0v = [0]*n
        w0v = [0]*n

        for i in range(n):

            u0v[i] = uvec[i] + 0.01234
            w0v[i] = wvec[i] - 0.05678

        uoutv, woutv, doutv = AxisProjVecPnt01Guess( geom_id, surf_indx, Y_DIR, ptvec, u0v,  w0v )

        for i in range(n):

            print( i, False )
            print( "U delta ", False )
            print( uvec[i] - uoutv[i], False )
            print( "W delta ", False )
            print( wvec[i] - woutv[i] )



    See also: AxisProjPnt01, AxisProjPnt01Guess, AxisProjPnt01I, AxisProjVecPnt01
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: iaxis int Axis direction to project point along (X_DIR, Y_DIR, or Z_DIR)
    :param [in]: pts vector<vec3d> Input vector of 3D coordinate points
    :param [in]: u0s vector<double> Input vector of U (0 - 1) surface coordinate guesses
    :param [in]: w0s vector<double> Input vector of W (0 - 1) surface coordinate guesses
    :param [out]: u_out_vec vector<double> Output vector of the closest U (0 - 1) surface coordinate for each 3D input point
    :param [out]: w_out_vec vector<double> Output vector of the closest W (0 - 1) surface coordinate for each 3D input point
    :param [out]: d_out_vec vector<double> Output vector of axis distances for each 3D point and the projected point of the surface
    """
    return _vsp.AxisProjVecPnt01Guess(geom_id, surf_indx, iaxis, pts, u0s, w0s)

@client_wrap
def VecInsideSurf(geom_id, surf_indx, pts):
    r"""
    Test whether a vector of points are inside a specified surface.



    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        n = 5

        rvec = [0]*n
        svec = [0]*n
        tvec = [0]*n

        for i in range(n):

            rvec[i] = (i+1)*1.0/(n+1)

            svec[i] = (n-i)*1.0/(n+1)

            tvec[i] = (i+1)*1.0/(n+1)

        ptvec = CompVecPntRST( geom_id, 0, rvec, svec, tvec )


        res = VecInsideSurf( geom_id, surf_indx, ptvec )



    See also: VecInsideSurf
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pts vector<vec3d> Input vector of 3D coordinate points
    :rtype: std::vector< bool,std::allocator< bool > >
    :return: Boolean vector for each point.  True if it is inside the surface, false otherwise.
    """
    return _vsp.VecInsideSurf(geom_id, surf_indx, pts)

@client_wrap
def CompVecPntRST(geom_id, surf_indx, r_in_vec, s_in_vec, t_in_vec):
    r"""
    Determine 3D coordinate for each volume coordinate point in the input arrays


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        rvec = [0]*n
        svec = [0]*n
        tvec = [0]*n

        for i in range(n):

            rvec[i] = (i+1)*1.0/(n+1)

            svec[i] = (n-i)*1.0/(n+1)

            tvec[i] = (i+1)*1.0/(n+1)

        ptvec = CompVecPntRST( geom_id, 0, rvec, svec, tvec )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: r_in_vec vector<double> Input vector of R (0 - 1.0) volume coordinates
    :param [in]: s_in_vec vector<double> Input vector of S (0 - 1.0) volume coordinates
    :param [in]: t_in_vec vector<double> Input vector of T (0 - 1.0) volume coordinates
    :rtype: std::vector< vec3d,std::allocator< vec3d > >
    :return: vector<vec3d> Vector of 3D coordinate points
    """
    return _vsp.CompVecPntRST(geom_id, surf_indx, r_in_vec, s_in_vec, t_in_vec)

@client_wrap
def FindRSTVec(geom_id, surf_indx, pts):
    r"""
    Determine the nearest volume coordinates for an input array of 3D coordinate points and calculate the distance between each
    3D point and the found point in the volume.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        rvec = [0]*n
        svec = [0]*n
        tvec = [0]*n

        for i in range(n):

            rvec[i] = (i+1)*1.0/(n+1)

            svec[i] = (n-i)*1.0/(n+1)

            tvec[i] = (i+1)*1.0/(n+1)

        ptvec = CompVecPntRST( geom_id, 0, rvec, svec, tvec )



        routv, soutv, toutv, doutv = FindRSTVec( geom_id, 0, ptvec )


    See also: FindRSTVecGuess
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pts vector<vec3d> Input vector of 3D coordinate points
    :param [out]: r_out_vec vector<double> Output vector of the closest R (0 - 1.0) volume coordinate for each 3D input point
    :param [out]: s_out_vec vector<double> Output vector of the closest S (0 - 1.0) volume coordinate for each 3D input point
    :param [out]: t_out_vec vector<double> Output vector of the closest T (0 - 1.0) volume coordinate for each 3D input point
    :param [out]: d_out_vec vector<double> Output vector of distances for each 3D point and the closest point of the volume
    """
    return _vsp.FindRSTVec(geom_id, surf_indx, pts)

@client_wrap
def FindRSTVecGuess(geom_id, surf_indx, pts, r0s, s0s, t0s):
    r"""
    Determine the nearest volume coordinates for an input array of 3D coordinate points and calculate the distance between each
    3D point and the closest point of the volume. This function takes an input array of volume coordinate guesses for each 3D
    coordinate, offering a potential decrease in computation time compared to FindRSTVec.


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        rvec = [0]*n
        svec = [0]*n
        tvec = [0]*n

        for i in range(n):

            rvec[i] = (i+1)*1.0/(n+1)

            svec[i] = (n-i)*1.0/(n+1)

            tvec[i] = (i+1)*1.0/(n+1)

        ptvec = CompVecPntRST( geom_id, 0, rvec, svec, tvec )

        for i in range(n):

            ptvec[i].set_xyz(ptvec[i].x() * 0.9, ptvec[i].y() * 0.9, ptvec[i].z() * 0.9)

         routv, soutv, toutv, doutv = FindRSTVecGuess( geom_id, 0, ptvec, rvec, svec, tvec )


    See also: FindRSTVec,
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: pts vector<vec3d> Input vector of 3D coordinate points
    :param [in]: r0s vector<double> Input vector of U (0 - 1.0) volume coordinate guesses
    :param [in]: s0s vector<double> Input vector of S (0 - 1.0) volume coordinate guesses
    :param [in]: t0s vector<double> Input vector of T (0 - 1.0) volume coordinate guesses
    :param [out]: r_out_vec vector<double> Output vector of the closest R (0 - 1.0) volume coordinate for each 3D input point
    :param [out]: s_out_vec vector<double> Output vector of the closest S (0 - 1.0) volume coordinate for each 3D input point
    :param [out]: t_out_vec vector<double> Output vector of the closest T (0 - 1.0) volume coordinate for each 3D input point
    :param [out]: d_out_vec vector<double> Output vector of distances for each 3D point and the closest point of the volume
    """
    return _vsp.FindRSTVecGuess(geom_id, surf_indx, pts, r0s, s0s, t0s)

@client_wrap
def ConvertRSTtoLMNVec(geom_id, surf_indx, r_vec, s_vec, t_vec):
    r"""
    Convert vector of RST volumetric coordinates to LMN coordinates.



    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        rvec = [0]*n
        svec = [0]*n
        tvec = [0]*n

        for i in range(n):

            rvec[i] = (i+1)*1.0/(n+1)
            svec[i] = (n-i)*1.0/(n+1)
            tvec[i] = (i+1)*1.0/(n+1)



        lvec, mvec, nvec = ConvertRSTtoLMNVec( geom_id, 0, rvec, svec, tvec )



    See also: ConvertLMNtoRSTVec, ConvertRSTtoLMN, ConvertLMNtoRST
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: r_vec vector<double> Input vector of R (0 - 1) volumetric coordinate
    :param [in]: s_vec vector<double> Input vector of S (0 - 1) volumetric coordinate
    :param [in]: t_vec vector<double> Input vector of T (0 - 1) volumetric coordinate
    :param [out]: l_out_vec vector<double> Output vector of L (0 - 1) linear volumetric coordinate
    :param [out]: m_out_vec vector<double> Output vector of M (0 - 1) linear volumetric coordinate
    :param [out]: n_out_vec vector<double> Output vector of N (0 - 1) linear volumetric coordinate
    """
    return _vsp.ConvertRSTtoLMNVec(geom_id, surf_indx, r_vec, s_vec, t_vec)

@client_wrap
def ConvertLMNtoRSTVec(geom_id, surf_indx, l_vec, m_vec, n_vec):
    r"""
    Convert vector of LMN volumetric coordinates to RST coordinates.



    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        n = 5

        lvec = [0]*n
        mvec = [0]*n
        nvec = [0]*n

        for i in range(n):

            lvec[i] = (i+1)*1.0/(n+1)
            mvec[i] = (n-i)*1.0/(n+1)
            nvec[i] = (i+1)*1.0/(n+1)

        rvec, svec, tvec = ConvertLMNtoRSTVec( geom_id, 0, lvec, mvec, nvec )



    See also: ConvertRSTtoLMNVec, ConvertRSTtoLMN, ConvertLMNtoRST
    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [in]: l_vec vector<double> Input vector of L (0 - 1) linear volumetric coordinate
    :param [in]: m_vec vector<double> Input vector of M (0 - 1) linear volumetric coordinate
    :param [in]: n_vec vector<double> Input vector of N (0 - 1) linear volumetric coordinate
    :param [out]: r_out_vec vector<double> Output vector of R (0 - 1) volumetric coordinate
    :param [out]: s_out_vec vector<double> Output vector of S (0 - 1) volumetric coordinate
    :param [out]: t_out_vec vector<double> Output vector of T (0 - 1) volumetric coordinate

    """
    return _vsp.ConvertLMNtoRSTVec(geom_id, surf_indx, l_vec, m_vec, n_vec)

@client_wrap
def GetUWTess01(geom_id, surf_indx):
    r"""
    Get the surface coordinate point of each intersection of the tessellated wireframe for a particular surface


    .. code-block:: python

        # Add Pod Geom
        geom_id = AddGeom( "POD", "" )

        surf_indx = 0

        utess, wtess = GetUWTess01( geom_id, surf_indx )


    :param [in]: geom_id string Parent Geom ID
    :param [in]: surf_indx int Main surface index from the parent Geom
    :param [out]: u_out_vec vector<double> Output vector of U (0 - 1) surface coordinates
    :param [out]: w_out_vec vector<double> Output vector of W (0 - 1) surface coordinates
    """
    return _vsp.GetUWTess01(geom_id, surf_indx)

@client_wrap
def AddRuler(startgeomid, startsurfindx, startu, startw, endgeomid, endsurfindx, endu, endw, name):
    r"""
    Create a new Ruler and add it to the Measure Tool


    .. code-block:: python

        pid1 = AddGeom( "POD", "" )

        SetParmVal( pid1, "Y_Rel_Location", "XForm", 2.0 )

        pid2 = AddGeom( "POD", "" )

        SetParmVal( pid2, "Z_Rel_Location", "XForm", 4.0 )

        rid = AddRuler( pid1, 1, 0.2, 0.3, pid2, 0, 0.2, 0.3, "Ruler 1" )

        SetParmVal( FindParm( rid, "X_Offset", "Measure" ), 6.0 )


    :param [in]: startgeomid string Start parent Geom ID
    :param [in]: startsurfindx int Main surface index from the staring parent Geom
    :param [in]: startu double Surface u (0 - 1) start coordinate
    :param [in]: startw double Surface w (0 - 1) start coordinate
    :param [in]: endgeomid string End parent Geom ID
    :param [in]: endsurfindx int Main surface index on the end parent Geom
    :param [in]: endu double Surface u (0 - 1) end coordinate
    :param [in]: endw double Surface w (0 - 1) end coordinate
    :param [in]: name string Ruler name
    :rtype: string
    :return: string Ruler ID
    """
    return _vsp.AddRuler(startgeomid, startsurfindx, startu, startw, endgeomid, endsurfindx, endu, endw, name)

@client_wrap
def GetAllRulers():
    r"""
    Get an array of all Ruler IDs from the Measure Tool


    .. code-block:: python

        pid1 = AddGeom( "POD", "" )

        SetParmVal( pid1, "Y_Rel_Location", "XForm", 2.0 )

        pid2 = AddGeom( "POD", "" )

        SetParmVal( pid2, "Z_Rel_Location", "XForm", 4.0 )

        rid1 = AddRuler( pid1, 1, 0.2, 0.3, pid2, 0, 0.2, 0.3, "Ruler 1" )

        rid2 = AddRuler( pid1, 0, 0.4, 0.6, pid1, 1, 0.8, 0.9, "Ruler 2" )

        ruler_array = GetAllRulers()

        print("Two Rulers")

        for n in range(len(ruler_array)):

            print( ruler_array[n] )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: vector<string> Vector of Ruler IDs
    """
    return _vsp.GetAllRulers()

@client_wrap
def DelRuler(id):
    r"""
    Delete a particular Ruler from the Measure Tool


    .. code-block:: python

        pid1 = AddGeom( "POD", "" )

        SetParmVal( pid1, "Y_Rel_Location", "XForm", 2.0 )

        pid2 = AddGeom( "POD", "" )

        SetParmVal( pid2, "Z_Rel_Location", "XForm", 4.0 )

        rid1 = AddRuler( pid1, 1, 0.2, 0.3, pid2, 0, 0.2, 0.3, "Ruler 1" )

        rid2 = AddRuler( pid1, 0, 0.4, 0.6, pid1, 1, 0.8, 0.9, "Ruler 2" )

        ruler_array = GetAllRulers()

        DelRuler( ruler_array[0] )


    :param [in]: id string Ruler ID
    """
    return _vsp.DelRuler(id)

@client_wrap
def DeleteAllRulers():
    r"""
    Delete all Rulers from the Measure Tool


    .. code-block:: python

        pid1 = AddGeom( "POD", "" )

        SetParmVal( pid1, "Y_Rel_Location", "XForm", 2.0 )

        pid2 = AddGeom( "POD", "" )

        SetParmVal( pid2, "Z_Rel_Location", "XForm", 4.0 )

        rid1 = AddRuler( pid1, 1, 0.2, 0.3, pid2, 0, 0.2, 0.3, "Ruler 1" )

        rid2 = AddRuler( pid1, 0, 0.4, 0.6, pid1, 1, 0.8, 0.9, "Ruler 2" )

        DeleteAllRulers()


    """
    return _vsp.DeleteAllRulers()

@client_wrap
def AddProbe(geomid, surfindx, u, w, name):
    r"""
    Create a new Probe and add it to the Measure Tool


    .. code-block:: python

        pid1 = AddGeom( "POD", "" )

        SetParmVal( pid1, "Y_Rel_Location", "XForm", 2.0 )

        probe_id = AddProbe( pid1, 0, 0.5, 0.8, "Probe 1" )

        SetParmVal( FindParm( probe_id, "Len", "Measure" ), 3.0 )


    :param [in]: geomid string Parent Geom ID
    :param [in]: surfindx int Main surface index from the parent Geom
    :param [in]: u double Surface u (0 - 1) coordinate
    :param [in]: w double Surface w (0 - 1) coordinate
    :param [in]: name string Probe name
    :rtype: string
    :return: string Probe ID
    """
    return _vsp.AddProbe(geomid, surfindx, u, w, name)

@client_wrap
def GetAllProbes():
    r"""
    Get an array of all Probe IDs from the Measure Tool


    .. code-block:: python

        pid1 = AddGeom( "POD", "" )

        SetParmVal( pid1, "Y_Rel_Location", "XForm", 2.0 )

        probe_id = AddProbe( pid1, 0, 0.5, 0.8, "Probe 1" )

        probe_array = GetAllProbes()

        print( "One Probe: ", False )

        print( probe_array[0] )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: [in] Array of Probe IDs
    """
    return _vsp.GetAllProbes()

@client_wrap
def DelProbe(id):
    r"""
    Delete a specific Probe from the Measure Tool


    .. code-block:: python

        pid1 = AddGeom( "POD", "" )

        SetParmVal( pid1, "Y_Rel_Location", "XForm", 2.0 )

        probe_id_1 = AddProbe( pid1, 0, 0.5, 0.8, "Probe 1" )
        probe_id_2 = AddProbe( pid1, 0, 0.2, 0.3, "Probe 2" )

        DelProbe( probe_id_1 )

        probe_array = GetAllProbes()

        if  len(probe_array) != 1 : print( "Error: DelProbe" )


    :param [in]: id Probe ID
    """
    return _vsp.DelProbe(id)

@client_wrap
def DeleteAllProbes():
    r"""
    Delete all Probes from the Measure Tool


    .. code-block:: python

        pid1 = AddGeom( "POD", "" )

        SetParmVal( pid1, "Y_Rel_Location", "XForm", 2.0 )

        probe_id_1 = AddProbe( pid1, 0, 0.5, 0.8, "Probe 1" )
        probe_id_2 = AddProbe( pid1, 0, 0.2, 0.3, "Probe 2" )

        DeleteAllProbes()

        probe_array = GetAllProbes()

        if  len(probe_array) != 0 : print( "Error: DeleteAllProbes" )


    """
    return _vsp.DeleteAllProbes()

@client_wrap
def GetAdvLinkNames():
    r"""
    Get an array of all advanced link names


    .. code-block:: python

        link_array = GetAdvLinkNames()

        for n in range(len(link_array) ):

            print( link_array[n] )


    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of advanced link names
    """
    return _vsp.GetAdvLinkNames()

@client_wrap
def GetLinkIndex(name):
    r"""
    Find the index of a specific advanced link.


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )



    :param [in]: name string Name for advanced link
    :rtype: int
    :return: index for advanced link

    """
    return _vsp.GetLinkIndex(name)

@client_wrap
def DelAdvLink(index):
    r"""
    Delete an advanced link specified by index


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        DelAdvLink( indx )

        link_array = GetAdvLinkNames()

        # Should print nothing.
        for n in range(len(link_array) ):

            print( link_array[n] )



    :param [in]: index Index for advanced link
    """
    return _vsp.DelAdvLink(index)

@client_wrap
def DelAllAdvLinks():
    r"""
    Delete all advanced links


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        DelAllAdvLinks()

        link_array = GetAdvLinkNames()

        # Should print nothing.
        for n in range( len(link_array) ):

            print( link_array[n] )



    """
    return _vsp.DelAllAdvLinks()

@client_wrap
def AddAdvLink(name):
    r"""
    Add an advanced link


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )



    :param [in]: name string Name for advanced link
    """
    return _vsp.AddAdvLink(name)

@client_wrap
def AddAdvLinkInput(index, parm_id, var_name):
    r"""
    Add an input variable to an advanced link


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )



    :param [in]: index int Advanced link index
    :param [in]: parm_id string Parameter ID for advanced link input variable
    :param [in]: var_name string Name for advanced link input variable
    """
    return _vsp.AddAdvLinkInput(index, parm_id, var_name)

@client_wrap
def AddAdvLinkOutput(index, parm_id, var_name):
    r"""
    Add an output variable to an advanced link


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )



    :param [in]: index int Advanced link index
    :param [in]: parm_id string Parameter ID for advanced link output variable
    :param [in]: var_name string Name for advanced link output variable
    """
    return _vsp.AddAdvLinkOutput(index, parm_id, var_name)

@client_wrap
def DelAdvLinkInput(index, var_name):
    r"""
    Delete an input variable from an advanced link


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )
        y_pos = GetParm( pod, "Y_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )
        AddAdvLinkInput( indx, y_pos, "y" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        DelAdvLinkInput( indx, "y" )

        BuildAdvLinkScript( indx )



    :param [in]: index int Advanced link index
    :param [in]: var_name string Name for advanced link input variable to delete
    """
    return _vsp.DelAdvLinkInput(index, var_name)

@client_wrap
def DelAdvLinkOutput(index, var_name):
    r"""
    Delete an output variable from an advanced link


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )
        y_pos = GetParm( pod, "Y_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )
        AddAdvLinkOutput( indx, y_pos, "y" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        DelAdvLinkOutput( indx, "y" )

        BuildAdvLinkScript( indx )



    :param [in]: index int Advanced link index
    :param [in]: var_name string Name for advanced link output variable to delete
    """
    return _vsp.DelAdvLinkOutput(index, var_name)

@client_wrap
def GetAdvLinkInputNames(index):
    r"""
    Get the name of all the inputs to a specified advanced link index


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        name_array = GetAdvLinkInputNames( indx )

        for n in range(len(name_array) ):

            print( name_array[n] )



    :param [in]: index int Advanced link index
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of advanced link input names
    """
    return _vsp.GetAdvLinkInputNames(index)

@client_wrap
def GetAdvLinkInputParms(index):
    r"""
    Get the Parm IDs of all the inputs to a specified advanced link index


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        parm_array = GetAdvLinkInputParms( indx )

        for n in range( len(parm_array) ):

            print( parm_array[n] )



    :param [in]: index int Advanced link index
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of advanced link input Parm IDs
    """
    return _vsp.GetAdvLinkInputParms(index)

@client_wrap
def GetAdvLinkOutputNames(index):
    r"""
    Get the Parm IDs of all the outputs to a specified advanced link index


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        name_array = GetAdvLinkOutputNames( indx )

        for n in range( len(name_array) ):

            print( name_array[n] )



    :param [in]: index int Advanced link index
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of advanced link output names
    """
    return _vsp.GetAdvLinkOutputNames(index)

@client_wrap
def GetAdvLinkOutputParms(index):
    r"""
    Get the Parm IDs of all the outputs to a specified advanced link index


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        parm_array = GetAdvLinkOutputParms( indx )

        for n in range( len(parm_array) ):

            print( parm_array[n] )



    :param [in]: index int Advanced link index
    :rtype: std::vector< std::string,std::allocator< std::string > >
    :return: Array of advanced link output Parm IDs
    """
    return _vsp.GetAdvLinkOutputParms(index)

@client_wrap
def ValidateAdvLinkParms(index):
    r"""
    Validate the input and output parameters for an advanced link


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        valid = ValidateAdvLinkParms( indx )

        if  valid :
            print( "Advanced link Parms are valid." )
        else:
            print( "Advanced link Parms are not valid." )



    :param [in]: index int Index for advanced link
    :rtype: boolean
    :return: Flag indicating whether parms are valid
    """
    return _vsp.ValidateAdvLinkParms(index)

@client_wrap
def SetAdvLinkCode(index, code):
    r"""
    Get the code from an advanced link


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )



    :param [in]: index int Index for advanced link
    :param [in]: code string Code for advanced link
    """
    return _vsp.SetAdvLinkCode(index, code)

@client_wrap
def GetAdvLinkCode(index):
    r"""
    Get the code from an advanced link


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        BuildAdvLinkScript( indx )

        code = GetAdvLinkCode( indx )

        print( code )



    :param [in]: index int Index for advanced link
    :rtype: string
    :return: String containing advanced link code
    """
    return _vsp.GetAdvLinkCode(index)

@client_wrap
def SearchReplaceAdvLinkCode(index, _from, to):
    r"""
    Search and replace strings in the advanced link code


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )
        SearchReplaceAdvLinkCode( indx, "10.0", "12.3" )

        code = GetAdvLinkCode( indx )

        print( code )

        BuildAdvLinkScript( indx )



    :param [in]: index int Index for advanced link
    :param [in]: from string Search token
    :param [in]: to string Replace token
    """
    return _vsp.SearchReplaceAdvLinkCode(index, _from, to)

@client_wrap
def BuildAdvLinkScript(index):
    r"""
    Build (ready for execution and perform syntax check) an advanced link.


    .. code-block:: python


        pod = AddGeom( "POD", "" )
        length = FindParm( pod, "Length", "Design" )
        x_pos = GetParm( pod, "X_Rel_Location", "XForm" )

        AddAdvLink( "ExampleLink" )
        indx = GetLinkIndex( "ExampleLink" )
        AddAdvLinkInput( indx, length, "len" )
        AddAdvLinkOutput( indx, x_pos, "x" )

        SetAdvLinkCode( indx, "x = 10.0 - len;" )

        success = BuildAdvLinkScript( indx )

        if  success :
            print( "Advanced link build successful." )
        else:
            print( "Advanced link build not successful." )



    :param [in]: index int Index for advanced link
    :rtype: boolean
    :return: Flag indicating whether advanced link build was successful
    """
    return _vsp.BuildAdvLinkScript(index)

@client_wrap
def AddVec3D(INOUT, x, y, z):
    r"""AddVec3D(Vec3dVec INOUT, double x, double y, double z)"""
    return _vsp.AddVec3D(INOUT, x, y, z)
cvar = _vsp.cvar

@client_wrap
def dist(a, b):
    r"""dist(vec3d a, vec3d b) -> double"""
    return _vsp.dist(a, b)

@client_wrap
def dist_squared(a, b):
    r"""dist_squared(vec3d a, vec3d b) -> double"""
    return _vsp.dist_squared(a, b)

@client_wrap
def dot(a, b):
    r"""dot(vec3d a, vec3d b) -> double"""
    return _vsp.dot(a, b)

@client_wrap
def cross(a, b):
    r"""cross(vec3d a, vec3d b) -> vec3d"""
    return _vsp.cross(a, b)

@client_wrap
def angle(a, b):
    r"""angle(vec3d a, vec3d b) -> double"""
    return _vsp.angle(a, b)

@client_wrap
def signed_angle(a, b, ref):
    r"""signed_angle(vec3d a, vec3d b, vec3d ref) -> double"""
    return _vsp.signed_angle(a, b, ref)

@client_wrap
def cos_angle(a, b):
    r"""cos_angle(vec3d a, vec3d b) -> double"""
    return _vsp.cos_angle(a, b)

@client_wrap
def radius_of_circle(p1, p2, p3):
    r"""radius_of_circle(vec3d p1, vec3d p2, vec3d p3) -> double"""
    return _vsp.radius_of_circle(p1, p2, p3)

@client_wrap
def center_of_circle(p1, p2, p3, center):
    r"""center_of_circle(vec3d p1, vec3d p2, vec3d p3, vec3d center)"""
    return _vsp.center_of_circle(p1, p2, p3, center)

@client_wrap
def dist_pnt_2_plane(org, norm, pnt):
    r"""dist_pnt_2_plane(vec3d org, vec3d norm, vec3d pnt) -> double"""
    return _vsp.dist_pnt_2_plane(org, norm, pnt)

@client_wrap
def dist_pnt_2_line(line_pt1, line_pt2, pnt):
    r"""dist_pnt_2_line(vec3d line_pt1, vec3d line_pt2, vec3d pnt) -> double"""
    return _vsp.dist_pnt_2_line(line_pt1, line_pt2, pnt)

@client_wrap
def proj_pnt_on_line_seg(line_pt1, line_pt2, pnt):
    r"""proj_pnt_on_line_seg(vec3d line_pt1, vec3d line_pt2, vec3d pnt) -> vec3d"""
    return _vsp.proj_pnt_on_line_seg(line_pt1, line_pt2, pnt)

@client_wrap
def proj_pnt_on_ray(line_pt1, line_pt2, pnt):
    r"""proj_pnt_on_ray(vec3d line_pt1, vec3d line_pt2, vec3d pnt) -> vec3d"""
    return _vsp.proj_pnt_on_ray(line_pt1, line_pt2, pnt)

@client_wrap
def proj_pnt_on_line(line_pt1, line_pt2, pnt):
    r"""proj_pnt_on_line(vec3d line_pt1, vec3d line_pt2, vec3d pnt) -> vec3d"""
    return _vsp.proj_pnt_on_line(line_pt1, line_pt2, pnt)

@client_wrap
def proj_pnt_to_plane(org, plane_ln1, plane_ln2, pnt):
    r"""proj_pnt_to_plane(vec3d org, vec3d plane_ln1, vec3d plane_ln2, vec3d pnt) -> vec3d"""
    return _vsp.proj_pnt_to_plane(org, plane_ln1, plane_ln2, pnt)

@client_wrap
def proj_vec_to_plane(vec, norm):
    r"""proj_vec_to_plane(vec3d vec, vec3d norm) -> vec3d"""
    return _vsp.proj_vec_to_plane(vec, norm)

@client_wrap
def tri_seg_intersect(A, B, C, D, E, u, w, t):
    r"""tri_seg_intersect(vec3d A, vec3d B, vec3d C, vec3d D, vec3d E, double & u, double & w, double & t) -> int"""
    return _vsp.tri_seg_intersect(A, B, C, D, E, u, w, t)

@client_wrap
def tri_ray_intersect(A, B, C, D, E, u, w, t):
    r"""tri_ray_intersect(vec3d A, vec3d B, vec3d C, vec3d D, vec3d E, double & u, double & w, double & t) -> int"""
    return _vsp.tri_ray_intersect(A, B, C, D, E, u, w, t)

@client_wrap
def plane_ray_intersect(*args):
    r"""
    plane_ray_intersect(vec3d A, vec3d B, vec3d C, vec3d D, vec3d E, double & t) -> int
    plane_ray_intersect(vec3d orig, vec3d norm, vec3d D, vec3d E, double & t) -> int
    """
    return _vsp.plane_ray_intersect(*args)

@client_wrap
def ray_ray_intersect(A, B, C, D, int_pnt1, int_pnt2):
    r"""ray_ray_intersect(vec3d A, vec3d B, vec3d C, vec3d D, vec3d int_pnt1, vec3d int_pnt2) -> int"""
    return _vsp.ray_ray_intersect(A, B, C, D, int_pnt1, int_pnt2)

@client_wrap
def tetra_volume(A, B, C):
    r"""tetra_volume(vec3d A, vec3d B, vec3d C) -> double"""
    return _vsp.tetra_volume(A, B, C)

@client_wrap
def area(A, B, C):
    r"""area(vec3d A, vec3d B, vec3d C) -> double"""
    return _vsp.area(A, B, C)

@client_wrap
def poly_area(pnt_vec):
    r"""poly_area(Vec3dVec pnt_vec) -> double"""
    return _vsp.poly_area(pnt_vec)

@client_wrap
def dist3D_Segment_to_Segment(*args):
    r"""
    dist3D_Segment_to_Segment(vec3d S1P0, vec3d S1P1, vec3d S2P0, vec3d S2P1) -> double
    dist3D_Segment_to_Segment(vec3d S1P0, vec3d S1P1, vec3d S2P0, vec3d S2P1, double * Lt, vec3d Ln, double * St, vec3d Sn) -> double
    """
    return _vsp.dist3D_Segment_to_Segment(*args)

@client_wrap
def nearSegSeg(L0, L1, S0, S1, Lt, Ln, St, Sn):
    r"""nearSegSeg(vec3d L0, vec3d L1, vec3d S0, vec3d S1, double * Lt, vec3d Ln, double * St, vec3d Sn) -> double"""
    return _vsp.nearSegSeg(L0, L1, S0, S1, Lt, Ln, St, Sn)

@client_wrap
def pointLineDistSquared(p, lp0, lp1, t):
    r"""pointLineDistSquared(vec3d p, vec3d lp0, vec3d lp1, double * t) -> double"""
    return _vsp.pointLineDistSquared(p, lp0, lp1, t)

@client_wrap
def pointSegDistSquared(p, sp0, sp1, t):
    r"""pointSegDistSquared(vec3d p, vec3d sp0, vec3d sp1, double * t) -> double"""
    return _vsp.pointSegDistSquared(p, sp0, sp1, t)

@client_wrap
def point_on_line(lp0, lp1, t):
    r"""point_on_line(vec3d lp0, vec3d lp1, double const & t) -> vec3d"""
    return _vsp.point_on_line(lp0, lp1, t)

@client_wrap
def MapToPlane(p, planeOrig, planeVec1, planeVec2):
    r"""MapToPlane(vec3d p, vec3d planeOrig, vec3d planeVec1, vec3d planeVec2) -> vec2d"""
    return _vsp.MapToPlane(p, planeOrig, planeVec1, planeVec2)

@client_wrap
def MapFromPlane(uw, planeOrig, planeVec1, planeVec2):
    r"""MapFromPlane(vec2d const & uw, vec3d planeOrig, vec3d planeVec1, vec3d planeVec2) -> vec3d"""
    return _vsp.MapFromPlane(uw, planeOrig, planeVec1, planeVec2)

@client_wrap
def plane_half_space(planeOrig, planeNorm, pnt):
    r"""plane_half_space(vec3d planeOrig, vec3d planeNorm, vec3d pnt) -> int"""
    return _vsp.plane_half_space(planeOrig, planeNorm, pnt)

@client_wrap
def line_line_intersect(p1, p2, p3, p4, s, t):
    r"""line_line_intersect(vec3d p1, vec3d p2, vec3d p3, vec3d p4, double * s, double * t) -> bool"""
    return _vsp.line_line_intersect(p1, p2, p3, p4, s, t)

@client_wrap
def RotateArbAxis(p, theta, r):
    r"""RotateArbAxis(vec3d p, double theta, vec3d r) -> vec3d"""
    return _vsp.RotateArbAxis(p, theta, r)

@client_wrap
def PtInTri(v0, v1, v2, p):
    r"""PtInTri(vec3d v0, vec3d v1, vec3d v2, vec3d p) -> bool"""
    return _vsp.PtInTri(v0, v1, v2, p)

@client_wrap
def BarycentricWeights(v0, v1, v2, p):
    r"""BarycentricWeights(vec3d v0, vec3d v1, vec3d v2, vec3d p) -> vec3d"""
    return _vsp.BarycentricWeights(v0, v1, v2, p)

@client_wrap
def BilinearWeights(p0, p1, p, weights):
    r"""BilinearWeights(vec3d p0, vec3d p1, vec3d p, DoubleVector weights)"""
    return _vsp.BilinearWeights(p0, p1, p, weights)

@client_wrap
def tri_tri_min_dist(v0, v1, v2, v3, v4, v5):
    r"""tri_tri_min_dist(vec3d v0, vec3d v1, vec3d v2, vec3d v3, vec3d v4, vec3d v5) -> double"""
    return _vsp.tri_tri_min_dist(v0, v1, v2, v3, v4, v5)

@client_wrap
def pnt_tri_min_dist(v0, v1, v2, pnt):
    r"""pnt_tri_min_dist(vec3d v0, vec3d v1, vec3d v2, vec3d pnt) -> double"""
    return _vsp.pnt_tri_min_dist(v0, v1, v2, pnt)

@client_wrap
def slerp(a, b, t):
    r"""slerp(vec3d a, vec3d b, double const & t) -> vec3d"""
    return _vsp.slerp(a, b, t)


@client_wrap
def to_string(v):
    r"""to_string(vec3d v) -> std::string"""
    return _vsp.to_string(v)

del _vsp
from openvsp.vsp import ErrorObj
from openvsp.vsp import ErrorMgrSingleton
from openvsp.vsp import vec3d
from openvsp.vsp import Matrix4d

# Facade Code
# **********************************************************************************
import os
import sys
import socket
from time import sleep
import subprocess
import pickle
from openvsp.facade_server import pack_data, unpack_data
from traceback import format_exception
import openvsp_config

# Starting the server
HOST = 'localhost'
PORT = 6000
server_file = os.path.join(os.path.dirname(os.path.abspath(__file__)), 'facade_server.py')
proc = subprocess.Popen([sys.executable, server_file, str(openvsp_config.LOAD_GRAPHICS)])

sleep(1)

sock = socket.socket(socket.AF_INET, socket.SOCK_STREAM)
sock.connect((HOST, PORT))

def _exception_hook(exc_type, exc_value, tb):
    regular_traceback = []
    facade_traceback = []
    for line in exc_value.args[0].split("\n")[:3]:
        facade_traceback.append(line)

    for line in format_exception(exc_type, exc_value, tb)[:-1]:
        if "facade.py" in line or "facade_server.py" in line:
            facade_traceback.append(line.strip("\n"))
        else:
            regular_traceback.append(line.strip("\n"))
    for line in exc_value.args[0].split("\n")[3:]:
        regular_traceback.append(line)

    print("This error occured while using the facade API")
    print("Facade Traceback:")
    for line in facade_traceback:
        print(line)
    print("")
    print("Regular Traceback:")
    for line in regular_traceback:
        print(line)

# function to send and recieve data from the facade server
def _send_recieve(func_name, args, kwargs):
    b_data = pack_data([func_name, args, kwargs], True)
    sock.sendall(b_data)
    result = None
    b_result = []
    while True:
        packet = sock.recv(202400)
        if not packet: break
        b_result.append(packet)
        try:
            result = unpack_data(b_result)
            break
        except:
            pass
    if isinstance(result, list) and result[0] == "error":
        sys.excepthook = _exception_hook
        raise Exception(result[1])
    return result

def IsFacade():
    """
    Returns True if the facade API is in use.


    .. code-block:: python

        is_facade = IsFacade()

    """

    return True
def IsGUIRunning():
    """
    Returns True if the GUI event loop is running.


    .. code-block:: python

        is_gui_active = IsGUIRunning()

    """

    return _send_recieve('IsGUIRunning', [], {})
