This group of API functions provides capabilities related to the body of revolution (BOR) geometry type in OpenVSP. Click here to return to the main page. More...

Functions
void	vsp::ChangeBORXSecShape (const std::string &bor_id, int type)
int	vsp::GetBORXSecShape (const std::string &bor_id)
std::vector< vec3d >	vsp::ReadBORFileXSec (const std::string &bor_id, const std::string &file_name)
std::vector< vec3d >	vsp::GetBORXSecPnts (const std::string &bor_id)
vec3d	vsp::ComputeBORXSecPnt (const std::string &bor_id, double fract)
vec3d	vsp::ComputeBORXSecTan (const std::string &bor_id, double fract)
void	vsp::ReadBORFileAirfoil (const std::string &bor_id, const std::string &file_name)
void	vsp::SetBORAirfoilUpperPnts (const std::string &bor_id, const std::vector< vec3d > &up_pnt_vec)
void	vsp::SetBORAirfoilLowerPnts (const std::string &bor_id, const std::vector< vec3d > &low_pnt_vec)
void	vsp::SetBORAirfoilPnts (const std::string &bor_id, const std::vector< vec3d > &up_pnt_vec, const std::vector< vec3d > &low_pnt_vec)
std::vector< vec3d >	vsp::GetBORAirfoilUpperPnts (const std::string &bor_id)
std::vector< vec3d >	vsp::GetBORAirfoilLowerPnts (const std::string &bor_id)
std::vector< double >	vsp::GetBORUpperCSTCoefs (const std::string &bor_id)
std::vector< double >	vsp::GetBORLowerCSTCoefs (const std::string &bor_id)
int	vsp::GetBORUpperCSTDegree (const std::string &bor_id)
int	vsp::GetBORLowerCSTDegree (const std::string &bor_id)
void	vsp::SetBORUpperCST (const std::string &bor_id, int deg, const std::vector< double > &coefs)
void	vsp::SetBORLowerCST (const std::string &bor_id, int deg, const std::vector< double > &coefs)
void	vsp::PromoteBORCSTUpper (const std::string &bor_id)
void	vsp::PromoteBORCSTLower (const std::string &bor_id)
void	vsp::DemoteBORCSTUpper (const std::string &bor_id)
void	vsp::DemoteBORCSTLower (const std::string &bor_id)
void	vsp::FitBORAfCST (const std::string &bor_id, int deg)

Detailed Description

Function Documentation

◆ ChangeBORXSecShape()

void vsp::ChangeBORXSecShape	(	const std::string &	bor_id,
		int	type )

extern

Set the XSec type for a BOR component

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_ROUNDED_RECTANGLE );
 
if ( GetBORXSecShape( bor_id ) != XS_ROUNDED_RECTANGLE ) { Print( "ERROR: ChangeBORXSecShape" ); __failure++; }

See also: XSEC_CRV_TYPE

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	type	int XSec type enum (i.e. XS_ROUNDED_RECTANGLE)

◆ ComputeBORXSecPnt()

vec3d vsp::ComputeBORXSecPnt	(	const std::string &	bor_id,
		double	fract )

extern

Compute 3D coordinate for a point on a BOR XSecCurve given the parameter value (U) along the curve

//==== Add Geom ====//
// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
double u_fract = 0.25;
 
vec3d pnt = ComputeBORXSecPnt( bor_id, u_fract );
 
// The section is a closed curve, so the ends meet.
if ( dist( ComputeBORXSecPnt( bor_id, 0.0 ), ComputeBORXSecPnt( bor_id, 1.0 ) ) > 1e-6 )
{
    Print( "ERROR: the BOR section does not close" );
    __failure++;
}
 
// The section lies in a plane of constant Z.
if ( !closeTo( pnt.z(), ComputeBORXSecPnt( bor_id, 0.0 ).z(), 1e-9 ) )
{
    Print( "ERROR: the BOR section is not planar" );
    __failure++;
}
 
// Walking the curve has to move, not sit still.
if ( dist( pnt, ComputeBORXSecPnt( bor_id, u_fract + 0.25 ) ) < 1e-9 )
{
    Print( "ERROR: ComputeBORXSecPnt does not advance along the curve" );
    __failure++;
}

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	fract	double Curve parameter value (range: 0 - 1)

Returns: vec3d Coordinate point on curve

◆ ComputeBORXSecTan()

vec3d vsp::ComputeBORXSecTan	(	const std::string &	bor_id,
		double	fract )

extern

Compute the tangent vector of a point on a BOR XSecCurve given the parameter value (U) along the curve

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
double u_fract = 0.25;
 
vec3d tan = ComputeBORXSecTan( bor_id, u_fract );
 
// A tangent is a direction, so it has to have some length.
if ( tan.mag() < 1e-9 )
{
    Print( "ERROR: ComputeBORXSecTan returned a degenerate tangent" );
    __failure++;
}
 
// The tangent has to follow the curve, so stepping along the curve from the
// point has to line up with it.
double du = 1.0e-5;
 
vec3d fd = ComputeBORXSecPnt( bor_id, u_fract + du ) - ComputeBORXSecPnt( bor_id, u_fract );
 
if ( fd.mag() < 1e-12 )
{
    Print( "ERROR: the BOR section does not advance" );
    __failure++;
}
else if ( dot( fd, tan ) / ( fd.mag() * tan.mag() ) < 0.999 )
{
    Print( "ERROR: ComputeBORXSecTan does not follow the curve" );
    __failure++;
}

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	fract	double Curve parameter value (range: 0 - 1)

Returns: vec3d Tangent vector on curve

◆ DemoteBORCSTLower()

void vsp::DemoteBORCSTLower ( const std::string & bor_id )

extern

Demote the CST for the lower airfoil surface of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL

See also: GetLowerCSTDegree

Parameters

[in] bor_id string Body of revolution Geom ID

◆ DemoteBORCSTUpper()

void vsp::DemoteBORCSTUpper ( const std::string & bor_id )

extern

Demote the CST for the upper airfoil surface of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL

See also: GetUpperCSTDegree

Parameters

[in] bor_id string Body of revolution Geom ID

◆ FitBORAfCST()

void vsp::FitBORAfCST	(	const std::string &	bor_id,
		int	deg )

extern

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.

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	deg	int CST degree

◆ GetBORAirfoilLowerPnts()

std::vector< vec3d > vsp::GetBORAirfoilLowerPnts ( const std::string & bor_id )

extern

Get the coordinate points for the lower surface of an airfoil of a BOR. The XSecCurve must be of type XS_FILE_AIRFOIL

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL );
 
ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" );
 
array< vec3d > @low_array = GetBORAirfoilLowerPnts( bor_id );
if ( low_array.length() == 0 )
{
    Print( "ERROR: GetBORAirfoilLowerPnts returned nothing" );
    __failure++;
}

See also: SetAirfoilPnts

Parameters

[in] bor_id string Body of revolution Geom ID

Returns: vector<vec3d> Vector of coordinate points for the lower airfoil surface

◆ GetBORAirfoilUpperPnts()

std::vector< vec3d > vsp::GetBORAirfoilUpperPnts ( const std::string & bor_id )

extern

Get the coordinate points for the upper surface of an airfoil on a BOR. The BOR XSecCurve must be of type XS_FILE_AIRFOIL

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL );
 
ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" );
 
array< vec3d > @up_array = GetBORAirfoilUpperPnts( bor_id );
if ( up_array.length() == 0 )
{
    Print( "ERROR: GetBORAirfoilUpperPnts returned nothing" );
    __failure++;
}

See also: SetAirfoilPnts

Parameters

[in] bor_id string Body of revolution Geom ID

Returns: vector<vec3d> Vector of coordinate points for the upper airfoil surface

◆ GetBORLowerCSTCoefs()

std::vector< double > vsp::GetBORLowerCSTCoefs ( const std::string & bor_id )

extern

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

Parameters

[in] bor_id string Body of revolution Geom ID

Returns: vector<double> Vector of CST coefficients for the lower airfoil surface

◆ GetBORLowerCSTDegree()

int vsp::GetBORLowerCSTDegree ( const std::string & bor_id )

extern

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

Parameters

[in] bor_id string Body of revolution Geom ID

Returns: int CST Degree for lower airfoil surface

◆ GetBORUpperCSTCoefs()

std::vector< double > vsp::GetBORUpperCSTCoefs ( const std::string & bor_id )

extern

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

Parameters

[in] bor_id string Body of revolution Geom ID

Returns: vector<double> Vector of CST coefficients for the upper airfoil surface

◆ GetBORUpperCSTDegree()

int vsp::GetBORUpperCSTDegree ( const std::string & bor_id )

extern

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

Parameters

[in] bor_id string Body of revolution Geom ID

Returns: int CST Degree for upper airfoil surface

◆ GetBORXSecPnts()

std::vector< vec3d > vsp::GetBORXSecPnts ( const std::string & bor_id )

extern

Set the coordinate points for a specific BOR. The BOR XSecCurve must be of type XS_FILE_FUSE.

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_FUSE );
 
array< vec3d > @vec_array = ReadBORFileXSec( bor_id, "TestXSec.fxs" );
 
Update();
 
vec3d before = ComputeBORXSecPnt( bor_id, 0.0 );
 
if ( vec_array.size() == 0 )
{
    Print( "ERROR: ReadBORFileXSec returned no points" );
    __failure++;
}
else
{
    vec_array[1] = vec_array[1] * 2.0;
    vec_array[3] = vec_array[3] * 2.0;
 
    SetBORXSecPnts( bor_id, vec_array );
 
    Update();
 
    vec3d after = ComputeBORXSecPnt( bor_id, 0.0 );
 
    // Points 1 and 3 are the top and bottom of the diamond read from file,
    // so doubling them doubles the height of the section while leaving its
    // width alone.  The section is normalized to the body diameter by its
    // height, so the section grows half as wide as it was.
    if ( !closeTo( after.x(), 0.5 * before.x(), 1e-6 ) )
    {
        Print( "ERROR: SetBORXSecPnts did not reshape the section" );
        __failure++;
    }
}

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	pnt_vec	vector<vec3d> Vector of XSec coordinate points

Get the coordinate points for a specific BOR. The BOR XSecCurve must be of type XS_FILE_FUSE. The points are returned normalized to the section's width and height.

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_FUSE );
 
array< vec3d > @vec_array = ReadBORFileXSec( bor_id, "TestXSec.fxs" );
 
// The points that were read are the points the section is carrying.
array< vec3d > @check_array = GetBORXSecPnts( bor_id );
 
if ( check_array.size() == 0 )
{
    Print( "ERROR: GetBORXSecPnts returned nothing" );
    __failure++;
}
else
{
    // The stored points are normalized, so they fit in the unit box, and the
    // curve closes on itself.
    for ( int i = 0; i < int( check_array.size() ); i++ )
    {
        if ( abs( check_array[i].x() ) > 0.5 + 1e-9 || abs( check_array[i].y() ) > 0.5 + 1e-9 )
        {
            Print( "ERROR: GetBORXSecPnts returned a point outside the unit box" );
            __failure++;
        }
    }
 
    if ( dist( check_array[0], check_array[check_array.size() - 1] ) > 1e-8 )
    {
        Print( "ERROR: GetBORXSecPnts returned an open curve" );
        __failure++;
    }
}

See also: SetBORXSecPnts, ReadBORFileXSec

Parameters

[in] bor_id string Body of revolution Geom ID

Returns: vector<vec3d> Vector of XSec coordinate points

◆ GetBORXSecShape()

int vsp::GetBORXSecShape ( const std::string & bor_id )

extern

Get the XSec type for a BOR component

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_ROUNDED_RECTANGLE );
 
if ( GetBORXSecShape( bor_id ) != XS_ROUNDED_RECTANGLE ) { Print( "ERROR: GetBORXSecShape" ); __failure++; }

Parameters

[in] bor_id string Body of revolution Geom ID

Returns: int XSec type enum (i.e. XS_ROUNDED_RECTANGLE)

◆ PromoteBORCSTLower()

void vsp::PromoteBORCSTLower ( const std::string & bor_id )

extern

Promote the CST for the lower airfoil surface of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL

See also: GetLowerCSTDegree

Parameters

[in] bor_id string Body of revolution Geom ID

◆ PromoteBORCSTUpper()

void vsp::PromoteBORCSTUpper ( const std::string & bor_id )

extern

Promote the CST for the upper airfoil surface of a BOR. The XSecCurve must be of type XS_CST_AIRFOIL

See also: GetUpperCSTDegree

Parameters

[in] bor_id string Body of revolution Geom ID

◆ ReadBORFileAirfoil()

void vsp::ReadBORFileAirfoil	(	const std::string &	bor_id,
		const std::string &	file_name )

extern

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.

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL );
 
ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" );
 
array< vec3d > @up_array = GetBORAirfoilUpperPnts( bor_id );
array< vec3d > @low_array = GetBORAirfoilLowerPnts( bor_id );
 
if ( up_array.size() == 0 || up_array.size() != low_array.size() )
{
    Print( "ERROR: ReadBORFileAirfoil did not read matching surfaces" );
    __failure++;
}
else
{
    // The points run from the leading edge to the trailing edge on a unit
    // chord, and a NACA 0012 is symmetric top to bottom.
    if ( !closeTo( up_array[0].x(), 0.0, 1e-6 ) ||
         !closeTo( up_array[up_array.size() - 1].x(), 1.0, 1e-6 ) )
    {
        Print( "ERROR: ReadBORFileAirfoil did not normalize the chord" );
        __failure++;
    }
 
    double max_up = 0.0;
 
    for ( int i = 0; i < int( up_array.size() ); i++ )
    {
        if ( !closeTo( low_array[i].y(), -up_array[i].y(), 1e-6 ) )
        {
            Print( "ERROR: ReadBORFileAirfoil did not read a symmetric section" );
            __failure++;
        }
 
        if ( up_array[i].y() > max_up )
        {
            max_up = up_array[i].y();
        }
    }
 
    if ( !closeTo( 2.0 * max_up, 0.12, 1e-3 ) )
    {
        Print( "ERROR: ReadBORFileAirfoil did not read a twelve percent section" );
        __failure++;
    }
}

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	file_name	string Airfoil XSec file name

◆ ReadBORFileXSec()

std::vector< vec3d > vsp::ReadBORFileXSec	(	const std::string &	bor_id,
		const std::string &	file_name )

extern

Set the coordinate points for a specific BOR. The BOR XSecCurve must be of type XS_FILE_FUSE.

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_FUSE );
 
array< vec3d > @vec_array = ReadBORFileXSec( bor_id, "TestXSec.fxs" );
 
Update();
 
// The file holds a closed curve, and the section it produced is the one the
// body is now built on.
if ( vec_array.size() < 3 )
{
    Print( "ERROR: ReadBORFileXSec returned too few points" );
    __failure++;
}
else if ( dist( vec_array[0], vec_array[vec_array.size() - 1] ) > 1e-8 )
{
    Print( "ERROR: ReadBORFileXSec returned an open curve" );
    __failure++;
}
 
if ( GetBORXSecShape( bor_id ) != XS_FILE_FUSE )
{
    Print( "ERROR: ReadBORFileXSec changed the section type" );
    __failure++;
}
 
// The section curve closes on itself.
if ( dist( ComputeBORXSecPnt( bor_id, 0.0 ), ComputeBORXSecPnt( bor_id, 1.0 ) ) > 1e-6 )
{
    Print( "ERROR: the BOR section does not close" );
    __failure++;
}

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	file_name	string Fuselage XSec file name

Returns: vector<vec3d> Array of coordinate points read from the file and set to the XSec

◆ SetBORAirfoilLowerPnts()

void vsp::SetBORAirfoilLowerPnts	(	const std::string &	bor_id,
		const std::vector< vec3d > &	low_pnt_vec )

extern

Set the lower points for an airfoil on a BOR. The BOR XSecCurve must be of type XS_FILE_AIRFOIL.

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL );
 
ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" );
 
array< vec3d > @low_array = GetBORAirfoilLowerPnts( bor_id );
 
for ( int i = 0 ; i < int( low_array.size() ) ; i++ )
{
    low_array[i].scale_y( 0.5 );
}
 
SetBORAirfoilLowerPnts( bor_id, low_array );
 
// The halved lower surface has to come back halved, and the upper surface
// has to be left alone.
array< vec3d > @check_array = GetBORAirfoilLowerPnts( bor_id );
array< vec3d > @up_array = GetBORAirfoilUpperPnts( bor_id );
 
if ( check_array.size() != low_array.size() )
{
    Print( "ERROR: SetBORAirfoilLowerPnts point count" );
    __failure++;
}
else
{
    double max_up = 0.0;
    double min_low = 0.0;
 
    for ( int i = 0; i < int( low_array.size() ); i++ )
    {
        if ( dist( check_array[i], low_array[i] ) > 1e-6 )
        {
            Print( "ERROR: SetBORAirfoilLowerPnts did not store point " + i );
            __failure++;
        }
 
        if ( up_array[i].y() > max_up ) { max_up = up_array[i].y(); }
        if ( check_array[i].y() < min_low ) { min_low = check_array[i].y(); }
    }
 
    if ( !closeTo( 0.5 * max_up, -min_low, 1e-6 ) )
    {
        Print( "ERROR: SetBORAirfoilLowerPnts did not leave the upper surface alone" );
        __failure++;
    }
}

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	low_pnt_vec	vector<vec3d> Vector of points defining the lower surface of the airfoil

◆ SetBORAirfoilPnts()

void vsp::SetBORAirfoilPnts	(	const std::string &	bor_id,
		const std::vector< vec3d > &	up_pnt_vec,
		const std::vector< vec3d > &	low_pnt_vec )

extern

Set the upper and lower points for an airfoil on a BOR. The BOR XSecCurve must be of type XS_FILE_AIRFOIL.

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL );
 
ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" );
 
array< vec3d > @up_array = GetBORAirfoilUpperPnts( bor_id );
 
array< vec3d > @low_array = GetBORAirfoilLowerPnts( bor_id );
 
for ( int i = 0 ; i < int( up_array.size() ) ; i++ )
{
    up_array[i].scale_y( 2.0 );
 
    low_array[i].scale_y( 0.5 );
}
 
SetBORAirfoilPnts( bor_id, up_array, low_array );
 
array< vec3d > @check_up = GetBORAirfoilUpperPnts( bor_id );
array< vec3d > @check_low = GetBORAirfoilLowerPnts( bor_id );
 
if ( check_up.size() != up_array.size() || check_low.size() != low_array.size() )
{
    Print( "ERROR: SetBORAirfoilPnts point count" );
    __failure++;
}
else
{
    double max_up = 0.0;
    double min_low = 0.0;
 
    for ( int i = 0; i < int( up_array.size() ); i++ )
    {
        if ( dist( check_up[i], up_array[i] ) > 1e-6 || dist( check_low[i], low_array[i] ) > 1e-6 )
        {
            Print( "ERROR: SetBORAirfoilPnts did not store point " + i );
            __failure++;
        }
 
        if ( check_up[i].y() > max_up ) { max_up = check_up[i].y(); }
        if ( check_low[i].y() < min_low ) { min_low = check_low[i].y(); }
    }
 
    // The section started symmetric; doubling the top and halving the
    // bottom leaves the top four times as deep as the bottom.
    if ( !closeTo( max_up, -4.0 * min_low, 1e-6 ) )
    {
        Print( "ERROR: SetBORAirfoilPnts did not scale the two surfaces apart" );
        __failure++;
    }
}

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	up_pnt_vec	vector<vec3d> Vector of points defining the upper surface of the airfoil
[in]	low_pnt_vec	vector<_>vec3d> Vector of points defining the lower surface of the airfoil

◆ SetBORAirfoilUpperPnts()

void vsp::SetBORAirfoilUpperPnts	(	const std::string &	bor_id,
		const std::vector< vec3d > &	up_pnt_vec )

extern

Set the upper points for an airfoil on a BOR. The BOR XSecCurve must be of type XS_FILE_AIRFOIL.

// Add Body of Recolution
string bor_id = AddGeom( "BODYOFREVOLUTION", "" );
 
ChangeBORXSecShape( bor_id, XS_FILE_AIRFOIL );
 
ReadBORFileAirfoil( bor_id, "airfoil/N0012_VSP.af" );
 
array< vec3d > @up_array = GetBORAirfoilUpperPnts( bor_id );
 
for ( int i = 0 ; i < int( up_array.size() ) ; i++ )
{
    up_array[i].scale_y( 2.0 );
}
 
SetBORAirfoilUpperPnts( bor_id, up_array );
 
// The doubled upper surface has to come back doubled, and the lower surface
// has to be left alone.
array< vec3d > @check_array = GetBORAirfoilUpperPnts( bor_id );
array< vec3d > @low_array = GetBORAirfoilLowerPnts( bor_id );
 
if ( check_array.size() != up_array.size() )
{
    Print( "ERROR: SetBORAirfoilUpperPnts point count" );
    __failure++;
}
else
{
    double max_up = 0.0;
    double min_low = 0.0;
 
    for ( int i = 0; i < int( up_array.size() ); i++ )
    {
        if ( dist( check_array[i], up_array[i] ) > 1e-6 )
        {
            Print( "ERROR: SetBORAirfoilUpperPnts did not store point " + i );
            __failure++;
        }
 
        if ( check_array[i].y() > max_up ) { max_up = check_array[i].y(); }
        if ( low_array[i].y() < min_low ) { min_low = low_array[i].y(); }
    }
 
    if ( !closeTo( max_up, -2.0 * min_low, 1e-6 ) )
    {
        Print( "ERROR: SetBORAirfoilUpperPnts did not leave the lower surface alone" );
        __failure++;
    }
}

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	up_pnt_vec	vector<vec3d> Vector of points defining the upper surface of the airfoil

◆ SetBORLowerCST()

void vsp::SetBORLowerCST	(	const std::string &	bor_id,
		int	deg,
		const std::vector< double > &	coefs )

extern

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

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	deg	int CST degree of lower airfoil surface
[in]	coefs	vector<double> Vector of CST coefficients for the lower airfoil surface

◆ SetBORUpperCST()

void vsp::SetBORUpperCST	(	const std::string &	bor_id,
		int	deg,
		const std::vector< double > &	coefs )

extern

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

Parameters

[in]	bor_id	string Body of revolution Geom ID
[in]	deg	int CST degree of upper airfoil surface
[in]	coefs	vector<double> Array of CST coefficients for the upper airfoil surface

Functions

Detailed Description

Function Documentation

◆ ChangeBORXSecShape()

◆ ComputeBORXSecPnt()

◆ ComputeBORXSecTan()

◆ DemoteBORCSTLower()

◆ DemoteBORCSTUpper()

◆ FitBORAfCST()

◆ GetBORAirfoilLowerPnts()

◆ GetBORAirfoilUpperPnts()

◆ GetBORLowerCSTCoefs()

◆ GetBORLowerCSTDegree()

◆ GetBORUpperCSTCoefs()

◆ GetBORUpperCSTDegree()

◆ GetBORXSecPnts()

◆ GetBORXSecShape()

◆ PromoteBORCSTLower()

◆ PromoteBORCSTUpper()

◆ ReadBORFileAirfoil()

◆ ReadBORFileXSec()

◆ SetBORAirfoilLowerPnts()

◆ SetBORAirfoilPnts()

◆ SetBORAirfoilUpperPnts()

◆ SetBORLowerCST()

◆ SetBORUpperCST()