#include <aeroelem.h>

Inheritance diagram for AerodynamicOutput:

Collaboration diagram for AerodynamicOutput:

Classes
struct	Aero_output

Public Types
enum	eOutput { AEROD_OUT_NONE = 0x0U, AEROD_OUT_STD = (ToBeOutput::OUTPUT_PRIVATE << 0), AEROD_OUT_PGAUSS = (ToBeOutput::OUTPUT_PRIVATE << 1), AEROD_OUT_NODE = (ToBeOutput::OUTPUT_PRIVATE << 2), AEROD_OUT_MASK = (AEROD_OUT_STD \| AEROD_OUT_PGAUSS \| AEROD_OUT_NODE) }

enum	{ OUTPUT_NONE = 0x0U, OUTPUT_GP_X = (ToBeOutput::OUTPUT_PRIVATE << 4), OUTPUT_GP_R = (ToBeOutput::OUTPUT_PRIVATE << 5), OUTPUT_GP_V = (ToBeOutput::OUTPUT_PRIVATE << 6), OUTPUT_GP_W = (ToBeOutput::OUTPUT_PRIVATE << 7), OUTPUT_GP_CONFIGURATION = (OUTPUT_GP_X \| OUTPUT_GP_R \| OUTPUT_GP_V \| OUTPUT_GP_W), OUTPUT_GP_F = (ToBeOutput::OUTPUT_PRIVATE << 8), OUTPUT_GP_M = (ToBeOutput::OUTPUT_PRIVATE << 9), OUTPUT_GP_FORCES = (OUTPUT_GP_F \| OUTPUT_GP_M), OUTPUT_DEFAULT = (OUTPUT_GP_F \| OUTPUT_GP_M), OUTPUT_GP_ALL = (ToBeOutput::OUTPUT_PRIVATE_MASK & (~AEROD_OUT_MASK)) }

Public Member Functions
	AerodynamicOutput (flag f, int iNP, OrientationDescription ood)

	~AerodynamicOutput (void)

void	SetOutputFlag (flag f, int iNP)

void	ResetIterator (void)

void	SetData (const Vec3 &v, const doublereal *pd, const Vec3 &X, const Mat3x3 &R, const Vec3 &V, const Vec3 &W, const Vec3 &F, const Vec3 &M)

AerodynamicOutput::eOutput	GetOutput (void) const

bool	IsOutput (void) const

bool	IsSTD (void) const

bool	IsPGAUSS (void) const

bool	IsNODE (void) const

Protected Attributes
flag	m_eOutput

OrientationDescription	od

std::vector< Aero_output >	OutputData

std::vector< Aero_output > ::iterator	OutputIter

Detailed Description

Definition at line 47 of file aeroelem.h.

Member Enumeration Documentation

anonymous enum

Enumerator
OUTPUT_NONE
OUTPUT_GP_X
OUTPUT_GP_R
OUTPUT_GP_V
OUTPUT_GP_W
OUTPUT_GP_CONFIGURATION
OUTPUT_GP_F
OUTPUT_GP_M
OUTPUT_GP_FORCES
OUTPUT_DEFAULT
OUTPUT_GP_ALL

Definition at line 60 of file aeroelem.h.

              {
                 OUTPUT_NONE = 0x0U,
 
                 OUTPUT_GP_X = (ToBeOutput::OUTPUT_PRIVATE << 4),
                 OUTPUT_GP_R = (ToBeOutput::OUTPUT_PRIVATE << 5),
                 OUTPUT_GP_V = (ToBeOutput::OUTPUT_PRIVATE << 6),
                 OUTPUT_GP_W = (ToBeOutput::OUTPUT_PRIVATE << 7),
                 OUTPUT_GP_CONFIGURATION = (OUTPUT_GP_X | OUTPUT_GP_R | OUTPUT_GP_V | OUTPUT_GP_W),
 
                 OUTPUT_GP_F = (ToBeOutput::OUTPUT_PRIVATE << 8),
                 OUTPUT_GP_M = (ToBeOutput::OUTPUT_PRIVATE << 9),
 
                 OUTPUT_GP_FORCES = (OUTPUT_GP_F | OUTPUT_GP_M),
 
                 OUTPUT_DEFAULT = (OUTPUT_GP_F | OUTPUT_GP_M),
 
                 OUTPUT_GP_ALL = (ToBeOutput::OUTPUT_PRIVATE_MASK & (~AEROD_OUT_MASK))
         };

enum AerodynamicOutput::eOutput

Enumerator
AEROD_OUT_NONE
AEROD_OUT_STD
AEROD_OUT_PGAUSS
AEROD_OUT_NODE
AEROD_OUT_MASK

Definition at line 49 of file aeroelem.h.

                      {
                 AEROD_OUT_NONE          = 0x0U,
 
                 AEROD_OUT_STD           = (ToBeOutput::OUTPUT_PRIVATE << 0),
                 AEROD_OUT_PGAUSS        = (ToBeOutput::OUTPUT_PRIVATE << 1),
                 AEROD_OUT_NODE          = (ToBeOutput::OUTPUT_PRIVATE << 2),
 
                 AEROD_OUT_MASK          = (AEROD_OUT_STD | AEROD_OUT_PGAUSS | AEROD_OUT_NODE)
         };

Constructor & Destructor Documentation

AerodynamicOutput::AerodynamicOutput	(	flag	f,
		int	iNP,
		OrientationDescription	ood
	)

Definition at line 50 of file aeroelem.cc.

References SetOutputFlag().

 : m_eOutput(f),
 od(ood)
 {
         SetOutputFlag(f, iNP);
 }

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AerodynamicOutput::~AerodynamicOutput ( void )

Definition at line 58 of file aeroelem.cc.

References NO_OP.

 {
         NO_OP;
 }

Member Function Documentation

AerodynamicOutput::eOutput AerodynamicOutput::GetOutput ( void ) const

Definition at line 125 of file aeroelem.cc.

References AEROD_OUT_MASK, and m_eOutput.

Referenced by IsNODE(), IsPGAUSS(), IsSTD(), AerodynamicBody::Output(), AerodynamicBeam::Output(), and AerodynamicBeam2::Output().

 {
         return eOutput(m_eOutput & AEROD_OUT_MASK);
 }

bool AerodynamicOutput::IsNODE ( void ) const

Definition at line 149 of file aeroelem.cc.

References AEROD_OUT_NODE, and GetOutput().

 {
         return GetOutput() == AEROD_OUT_NODE;
 }

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bool AerodynamicOutput::IsOutput ( void ) const

Definition at line 131 of file aeroelem.cc.

References m_eOutput, and ToBeOutput::OUTPUT.

Referenced by ResetIterator(), and SetOutputFlag().

 {
         return (m_eOutput & ToBeOutput::OUTPUT);
 }

bool AerodynamicOutput::IsPGAUSS ( void ) const

Definition at line 143 of file aeroelem.cc.

References AEROD_OUT_PGAUSS, and GetOutput().

Referenced by ResetIterator(), SetData(), and SetOutputFlag().

 {
         return GetOutput() == AEROD_OUT_PGAUSS;
 }

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bool AerodynamicOutput::IsSTD ( void ) const

Definition at line 137 of file aeroelem.cc.

References AEROD_OUT_STD, and GetOutput().

 {
         return GetOutput() == AEROD_OUT_STD;
 }

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void AerodynamicOutput::ResetIterator ( void )

Definition at line 77 of file aeroelem.cc.

References ASSERT, IsOutput(), IsPGAUSS(), OutputData, and OutputIter.

Referenced by AerodynamicBody::AssJac(), AerodynamicBeam::AssJac(), AerodynamicBeam2::AssJac(), AerodynamicBody::AssVec(), AerodynamicBeam::AssVec(), and AerodynamicBeam2::AssVec().

 {
         if (IsOutput() && IsPGAUSS()) {
                 ASSERT(!OutputData.empty());
                 OutputIter = OutputData.begin();
         }
 
 #ifdef USE_NETCDF
         if (!NetCDFOutputData.empty()) {
                 NetCDFOutputIter = NetCDFOutputData.begin();
         }
 #endif // USE_NETCDF
 }

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void AerodynamicOutput::SetData	(	const Vec3 &	v,
		const doublereal *	pd,
		const Vec3 &	X,
		const Mat3x3 &	R,
		const Vec3 &	V,
		const Vec3 &	W,
		const Vec3 &	F,
		const Vec3 &	M
	)

Definition at line 92 of file aeroelem.cc.

References ASSERT, grad::atan2(), IsPGAUSS(), M_PI, OutputData, OutputIter, and R.

Referenced by AerodynamicBody::AssVec(), AerodynamicBeam::AssVec(), and AerodynamicBeam2::AssVec().

 {
         if (IsPGAUSS()) {
                 ASSERT(!OutputData.empty());
                 ASSERT(OutputIter >= OutputData.begin());
                 ASSERT(OutputIter < OutputData.end());
 
                 OutputIter->alpha = 180./M_PI*atan2(-v(2), v(1));
                 OutputIter->f = Vec3(pd[1], pd[0], pd[5]);
 
                 // move iterator forward
                 ++OutputIter;
         }
 
 #ifdef USE_NETCDF
         if (!NetCDFOutputData.empty()) {
                 ASSERT(NetCDFOutputIter >= NetCDFOutputData.begin());
                 ASSERT(NetCDFOutputIter < NetCDFOutputData.end());
 
                 if (NetCDFOutputIter->Var_X) NetCDFOutputIter->X = X;
                 if (NetCDFOutputIter->Var_Phi) NetCDFOutputIter->R = R;
                 if (NetCDFOutputIter->Var_V) NetCDFOutputIter->V = V;
                 if (NetCDFOutputIter->Var_W) NetCDFOutputIter->W = W;
                 if (NetCDFOutputIter->Var_F) NetCDFOutputIter->F = F;
                 if (NetCDFOutputIter->Var_M) NetCDFOutputIter->M = M;
 
                 ++NetCDFOutputIter;
         }
 #endif // USE_NETCDF
 }

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void AerodynamicOutput::SetOutputFlag	(	flag	f,
		int	iNP
	)

Definition at line 64 of file aeroelem.cc.

References IsOutput(), IsPGAUSS(), m_eOutput, and OutputData.

Referenced by AerodynamicOutput(), and Aerodynamic2DElem< iNN >::SetOutputFlag().

 {
         m_eOutput = f;
 
         if (IsOutput() && IsPGAUSS()) {
                 OutputData.resize(iNP);
 
         } else {
                 OutputData.resize(0);
         }
 }