CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray Struct Reference

Auxilary types to store common aero coefficients (avoids repeating oneself so much). More...

#include <CFVMFlowSolverBase.hpp>

Public Member Functions
void	allocate (int size)
	Allocates arrays.
void	setZero (int i)
	Sets all values to zero for all indices.
void	setZero ()
	AeroCoeffsArray (int size=0)
	~AeroCoeffsArray ()

Public Attributes
su2double *	CD = nullptr
	Drag coefficient.
su2double *	CL = nullptr
	Lift coefficient.
su2double *	CSF = nullptr
	Sideforce coefficient.
su2double *	CEff = nullptr
	Efficiency (Cl/Cd).
su2double *	CFx = nullptr
	x Force coefficient.
su2double *	CFy = nullptr
	y Force coefficient.
su2double *	CFz = nullptr
	z Force coefficient.
su2double *	CMx = nullptr
	x Moment coefficient.
su2double *	CMy = nullptr
	y Moment coefficient.
su2double *	CMz = nullptr
	z Moment coefficient.
su2double *	CoPx = nullptr
	x Moment coefficient.
su2double *	CoPy = nullptr
	y Moment coefficient.
su2double *	CoPz = nullptr
	z Moment coefficient.
su2double *	CT = nullptr
	Thrust coefficient.
su2double *	CQ = nullptr
	Torque coefficient.
su2double *	CMerit = nullptr
	Rotor Figure of Merit.
int	_size = 0
	Array size.

Detailed Description

template<class VariableType, ENUM_REGIME FlowRegime>
struct CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray

Auxilary types to store common aero coefficients (avoids repeating oneself so much).

Constructor & Destructor Documentation

AeroCoeffsArray()

template<class VariableType , ENUM_REGIME FlowRegime>

CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::AeroCoeffsArray ( int  size = 0 )

inline

~AeroCoeffsArray()

template<class V , ENUM_REGIME R>

CFVMFlowSolverBase< V, R >::AeroCoeffsArray::~AeroCoeffsArray

(

)

Member Function Documentation

allocate()

template<class V , ENUM_REGIME R>

void CFVMFlowSolverBase< V, R >::AeroCoeffsArray::allocate

(

int

size

)

Allocates arrays.

Sets all values to zero at a particular index.

setZero() [1/2]

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::setZero ( )

inline

setZero() [2/2]

template<class VariableType , ENUM_REGIME FlowRegime>

void CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::setZero ( int  i )

inline

Sets all values to zero for all indices.

Member Data Documentation

_size

template<class VariableType , ENUM_REGIME FlowRegime>

int CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::_size = 0

Array size.

CD

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CD = nullptr

Drag coefficient.

CEff

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CEff = nullptr

Efficiency (Cl/Cd).

CFx

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CFx = nullptr

x Force coefficient.

CFy

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CFy = nullptr

y Force coefficient.

CFz

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CFz = nullptr

z Force coefficient.

CL

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CL = nullptr

Lift coefficient.

CMerit

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CMerit = nullptr

Rotor Figure of Merit.

CMx

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CMx = nullptr

x Moment coefficient.

CMy

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CMy = nullptr

y Moment coefficient.

CMz

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CMz = nullptr

z Moment coefficient.

CoPx

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CoPx = nullptr

x Moment coefficient.

CoPy

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CoPy = nullptr

y Moment coefficient.

CoPz

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CoPz = nullptr

z Moment coefficient.

CQ

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CQ = nullptr

Torque coefficient.

CSF

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CSF = nullptr

Sideforce coefficient.

CT

template<class VariableType , ENUM_REGIME FlowRegime>

su2double* CFVMFlowSolverBase< VariableType, FlowRegime >::AeroCoeffsArray::CT = nullptr

Thrust coefficient.

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

• SU2_CFD/include/solvers/CFVMFlowSolverBase.hpp
• SU2_CFD/include/solvers/CFVMFlowSolverBase.inl