wsf::six_dof::AeroCoreObject Class Reference

#include <WsfSixDOF_AeroCoreObject.hpp>

Inheritance diagram for wsf::six_dof::AeroCoreObject:

Public Member Functions
	AeroCoreObject ()=default
	~AeroCoreObject ()=default
AeroCoreObject &	operator= (const AeroCoreObject &other)=delete
virtual bool	Initialize ()
void	SetModeName (const std::string &aName)
std::string	GetModeName () const
double	GetRefArea_sqft () const
double	CL_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad)
double	Cd_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad)
double	CY_AlphaBetaMach (double aMach, double aAlpha_rad, double aBeta_rad)
double	CalculateAeroCLArea (double aMach, double aAlpha_rad)
double	CalculateAeroCdArea (double aMach, double aAlpha_rad)

Protected Member Functions
	AeroCoreObject (const AeroCoreObject &aSrc)=default

Protected Attributes
std::string	mModeName = "DEFAULT"
double	mRefArea_sqft = 0.0
UtCloneablePtr< UtTable::Table >	mCL_AlphaBetaMachTablePtr {nullptr}
UtCloneablePtr< UtTable::Table >	mCd_AlphaBetaMachTablePtr {nullptr}
UtCloneablePtr< UtTable::Table >	mCY_AlphaBetaMachTablePtr {nullptr}

Constructor & Destructor Documentation

AeroCoreObject() [1/2]

wsf::six_dof::AeroCoreObject::AeroCoreObject ( )

default

Referenced by AeroCoreObject(), and operator=().

~AeroCoreObject()

wsf::six_dof::AeroCoreObject::~AeroCoreObject ( )

default

AeroCoreObject() [2/2]

wsf::six_dof::AeroCoreObject::AeroCoreObject ( const AeroCoreObject & aSrc )

protecteddefault

References AeroCoreObject().

Member Function Documentation

CalculateAeroCdArea()

double wsf::six_dof::AeroCoreObject::CalculateAeroCdArea	(	double	aMach,
		double	aAlpha_rad )

References Cd_AlphaBetaMach(), and mRefArea_sqft.

Referenced by wsf::six_dof::PointMassMoverTestObject::CalcLevelFlightDragAndAlpha(), and operator=().

CalculateAeroCLArea()

double wsf::six_dof::AeroCoreObject::CalculateAeroCLArea	(	double	aMach,
		double	aAlpha_rad )

References CL_AlphaBetaMach(), and mRefArea_sqft.

Referenced by operator=().

Cd_AlphaBetaMach()

double wsf::six_dof::AeroCoreObject::Cd_AlphaBetaMach	(	double	aMach,
		double	aAlpha_rad,
		double	aBeta_rad )

References mCd_AlphaBetaMachTablePtr.

Referenced by CalculateAeroCdArea(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateAeroCdArea(), wsf::six_dof::PointMassAeroCoreObject::CalculateAeroCoefficientVectors(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateAeroCoefficientVectors(), wsf::six_dof::PointMassAeroCoreObject::CalculateCoreAeroFM(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateCoreAeroFM(), and operator=().

CL_AlphaBetaMach()

double wsf::six_dof::AeroCoreObject::CL_AlphaBetaMach	(	double	aMach,
		double	aAlpha_rad,
		double	aBeta_rad )

References mCL_AlphaBetaMachTablePtr.

Referenced by CalculateAeroCLArea(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateAeroCLArea(), wsf::six_dof::PointMassAeroCoreObject::CalculateAeroCoefficientVectors(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateAeroCoefficientVectors(), wsf::six_dof::PointMassAeroCoreObject::CalculateCoreAeroFM(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateCoreAeroFM(), wsf::six_dof::PointMassAeroCoreObject::CalculateLiftAtSpecifiedAlpha_lbs(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateLiftAtSpecifiedAlpha_lbs(), and operator=().

CY_AlphaBetaMach()

double wsf::six_dof::AeroCoreObject::CY_AlphaBetaMach	(	double	aMach,
		double	aAlpha_rad,
		double	aBeta_rad )

References mCY_AlphaBetaMachTablePtr.

Referenced by wsf::six_dof::PointMassAeroCoreObject::CalculateCoreAeroFM(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateCoreAeroFM(), and operator=().

GetModeName()

std::string wsf::six_dof::AeroCoreObject::GetModeName

(

)

const

References mModeName.

Referenced by operator=().

GetRefArea_sqft()

double wsf::six_dof::AeroCoreObject::GetRefArea_sqft

(

)

const

References mRefArea_sqft.

Referenced by wsf::six_dof::RigidBodyMover::CalculateTotalCmAndCL(), and operator=().

Initialize()

bool wsf::six_dof::AeroCoreObject::Initialize ( )

virtual

Reimplemented in wsf::six_dof::RigidBodyAeroCoreObject.

Referenced by operator=().

operator=()

AeroCoreObject & wsf::six_dof::AeroCoreObject::operator= ( const AeroCoreObject & other )

delete

References AeroCoreObject(), CalculateAeroCdArea(), CalculateAeroCLArea(), Cd_AlphaBetaMach(), CL_AlphaBetaMach(), CY_AlphaBetaMach(), GetModeName(), GetRefArea_sqft(), Initialize(), and SetModeName().

SetModeName()

void wsf::six_dof::AeroCoreObject::SetModeName

(

const std::string &

aName

)

References mModeName.

Referenced by operator=().

Member Data Documentation

mCd_AlphaBetaMachTablePtr

UtCloneablePtr<UtTable::Table> wsf::six_dof::AeroCoreObject::mCd_AlphaBetaMachTablePtr {nullptr}

protected

Referenced by Cd_AlphaBetaMach(), wsf::six_dof::PointMassAeroCoreObject::ProcessCommonInput(), and wsf::six_dof::RigidBodyAeroCoreObject::ProcessCommonInput().

mCL_AlphaBetaMachTablePtr

UtCloneablePtr<UtTable::Table> wsf::six_dof::AeroCoreObject::mCL_AlphaBetaMachTablePtr {nullptr}

protected

Referenced by CL_AlphaBetaMach(), wsf::six_dof::PointMassAeroCoreObject::ProcessCommonInput(), and wsf::six_dof::RigidBodyAeroCoreObject::ProcessCommonInput().

mCY_AlphaBetaMachTablePtr

UtCloneablePtr<UtTable::Table> wsf::six_dof::AeroCoreObject::mCY_AlphaBetaMachTablePtr {nullptr}

protected

Referenced by CY_AlphaBetaMach(), wsf::six_dof::PointMassAeroCoreObject::ProcessCommonInput(), and wsf::six_dof::RigidBodyAeroCoreObject::ProcessCommonInput().

mModeName

std::string wsf::six_dof::AeroCoreObject::mModeName = "DEFAULT"

protected

Referenced by GetModeName(), wsf::six_dof::RigidBodyAeroCoreObject::GetModeName(), SetModeName(), and wsf::six_dof::RigidBodyAeroCoreObject::SetModeName().

mRefArea_sqft

double wsf::six_dof::AeroCoreObject::mRefArea_sqft = 0.0

protected

Referenced by CalculateAeroCdArea(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateAeroCdArea(), CalculateAeroCLArea(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateAeroCLArea(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateAeroCmArea(), wsf::six_dof::PointMassAeroCoreObject::CalculateAeroCoefficientVectors(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateAeroCoefficientVectors(), wsf::six_dof::PointMassAeroCoreObject::CalculateCoreAeroFM(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateCoreAeroFM(), wsf::six_dof::PointMassAeroCoreObject::CalculateLiftAtSpecifiedAlpha_lbs(), wsf::six_dof::RigidBodyAeroCoreObject::CalculateLiftAtSpecifiedAlpha_lbs(), GetRefArea_sqft(), wsf::six_dof::PointMassAeroCoreObject::ProcessCommonInput(), and wsf::six_dof::RigidBodyAeroCoreObject::ProcessCommonInput().

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The documentation for this class was generated from the following files:

• WsfSixDOF_AeroCoreObject.hpp
• WsfSixDOF_AeroCoreObject.cpp