Aerodynamic2DElem< iNN > Class Template Reference

#include <aeroelem.h>

Inheritance diagram for Aerodynamic2DElem< iNN >:

Collaboration diagram for Aerodynamic2DElem< iNN >:

Public Member Functions
	Aerodynamic2DElem (unsigned int uLabel, const DofOwner *pDO, InducedVelocity *pR, bool bPassive, const Shape *pC, const Shape *pF, const Shape *pV, const Shape *pT, const Shape *pTL, integer iN, AeroData *a, const DriveCaller *pDC, bool bUseJacobian, OrientationDescription ood, flag fOut)
virtual	~Aerodynamic2DElem (void)
virtual Elem::Type	GetElemType (void) const
virtual unsigned int	iGetNumDof (void) const
virtual std::ostream &	DescribeDof (std::ostream &out, const char *prefix="", bool bInitial=false) const
virtual void	DescribeDof (std::vector< std::string > &desc, bool bInitial=false, int i=-1) const
virtual std::ostream &	DescribeEq (std::ostream &out, const char *prefix="", bool bInitial=false) const
virtual void	DescribeEq (std::vector< std::string > &desc, bool bInitial=false, int i=-1) const
virtual DofOrder::Order	GetDofType (unsigned int) const
virtual void	OutputPrepare (OutputHandler &OH)
virtual void	SetValue (DataManager *pDM, VectorHandler &X, VectorHandler &XP, SimulationEntity::Hints *h=0)
virtual void	AfterConvergence (const VectorHandler &X, const VectorHandler &XP)
virtual void	WorkSpaceDim (integer *piNumRows, integer *piNumCols) const
virtual unsigned int	iGetInitialNumDof (void) const
virtual void	InitialWorkSpaceDim (integer *piNumRows, integer *piNumCols) const
virtual VariableSubMatrixHandler &	InitialAssJac (VariableSubMatrixHandler &WorkMat, const VectorHandler &)
virtual const InducedVelocity *	pGetInducedVelocity (void) const
Public Member Functions inherited from Elem
	Elem (unsigned int uL, flag fOut)
virtual	~Elem (void)
virtual std::ostream &	Restart (std::ostream &out) const =0
virtual void	AssMats (VariableSubMatrixHandler &WorkMatA, VariableSubMatrixHandler &WorkMatB, const VectorHandler &XCurr, const VectorHandler &XPrimeCurr)
virtual SubVectorHandler &	AssRes (SubVectorHandler &WorkVec, doublereal dCoef, const VectorHandler &XCurr, const VectorHandler &XPrimeCurr)=0
virtual VariableSubMatrixHandler &	AssJac (VariableSubMatrixHandler &WorkMat, doublereal dCoef, const VectorHandler &XCurr, const VectorHandler &XPrimeCurr)=0
virtual bool	bInverseDynamics (void) const
void	SetInverseDynamicsFlags (unsigned uIDF)
unsigned	GetInverseDynamicsFlags (void) const
bool	bIsErgonomy (void) const
bool	bIsRightHandSide (void) const
virtual VariableSubMatrixHandler &	AssJac (VariableSubMatrixHandler &WorkMat, const VectorHandler &XCurr)
virtual SubVectorHandler &	AssRes (SubVectorHandler &WorkVec, const VectorHandler &XCurr, const VectorHandler &XPrimeCurr, const VectorHandler &XPrimePrimeCurr, InverseDynamics::Order iOrder=InverseDynamics::INVERSE_DYNAMICS)
virtual int	GetNumConnectedNodes (void) const
virtual void	GetConnectedNodes (std::vector< const Node * > &connectedNodes) const
Public Member Functions inherited from WithLabel
	WithLabel (unsigned int uL=0, const std::string &sN="")
virtual	~WithLabel (void)
void	PutLabel (unsigned int uL)
void	PutName (const std::string &sN)
unsigned int	GetLabel (void) const
const std::string &	GetName (void) const
Public Member Functions inherited from SimulationEntity
	SimulationEntity (void)
virtual	~SimulationEntity (void)
virtual bool	bIsValidIndex (unsigned int i) const
virtual DofOrder::Order	GetEqType (unsigned int i) const
virtual Hint *	ParseHint (DataManager *pDM, const char *s) const
virtual void	BeforePredict (VectorHandler &, VectorHandler &, VectorHandler &, VectorHandler &) const
virtual void	AfterPredict (VectorHandler &X, VectorHandler &XP)
virtual void	Update (const VectorHandler &XCurr, const VectorHandler &XPrimeCurr)
virtual void	DerivativesUpdate (const VectorHandler &XCurr, const VectorHandler &XPrimeCurr)
virtual void	Update (const VectorHandler &XCurr, InverseDynamics::Order iOrder)
virtual void	AfterConvergence (const VectorHandler &X, const VectorHandler &XP, const VectorHandler &XPP)
virtual unsigned int	iGetNumPrivData (void) const
virtual unsigned int	iGetPrivDataIdx (const char *s) const
virtual doublereal	dGetPrivData (unsigned int i) const
virtual std::ostream &	OutputAppend (std::ostream &out) const
virtual void	ReadInitialState (MBDynParser &HP)
Public Member Functions inherited from ToBeOutput
	ToBeOutput (flag fOut=fDefaultOut)
virtual	~ToBeOutput (void)
virtual void	Output (OutputHandler &OH) const
virtual void	Output (OutputHandler &OH, const VectorHandler &X, const VectorHandler &XP) const
virtual flag	fToBeOutput (void) const
virtual bool	bToBeOutput (void) const
Public Member Functions inherited from AerodynamicElem
	AerodynamicElem (unsigned int uL, const DofOwner *pDO, flag fOut)
virtual	~AerodynamicElem (void)
virtual AerodynamicElem::Type	GetAerodynamicElemType (void) const =0
virtual bool	NeedsAirProperties (void) const
Public Member Functions inherited from ElemWithDofs
	ElemWithDofs (unsigned int uL, const DofOwner *pDO, flag fOut)
virtual	~ElemWithDofs (void)
Public Member Functions inherited from DofOwnerOwner
	DofOwnerOwner (const DofOwner *pDO)
virtual	~DofOwnerOwner ()
virtual const DofOwner *	pGetDofOwner (void) const
virtual integer	iGetFirstIndex (void) const
virtual void	SetInitialValue (VectorHandler &X)
Public Member Functions inherited from AirPropOwner
	AirPropOwner (void)
virtual	~AirPropOwner (void)
virtual void	PutAirProperties (const AirProperties *pAP)
virtual flag	fGetAirVelocity (Vec3 &Velocity, const Vec3 &X) const
virtual doublereal	dGetAirDensity (const Vec3 &X) const
virtual doublereal	dGetAirPressure (const Vec3 &X) const
virtual doublereal	dGetAirTemperature (const Vec3 &X) const
virtual doublereal	dGetSoundSpeed (const Vec3 &X) const
virtual bool	GetAirProps (const Vec3 &X, doublereal &rho, doublereal &c, doublereal &p, doublereal &T) const
Public Member Functions inherited from InitialAssemblyElem
	InitialAssemblyElem (unsigned int uL, flag fOut)
virtual	~InitialAssemblyElem (void)
Public Member Functions inherited from SubjectToInitialAssembly
	SubjectToInitialAssembly (void)
virtual	~SubjectToInitialAssembly (void)
virtual SubVectorHandler &	InitialAssRes (SubVectorHandler &WorkVec, const VectorHandler &XCurr)=0
Public Member Functions inherited from DriveOwner
	DriveOwner (const DriveCaller *pDC=0)
	DriveOwner (const DriveOwner &drive)
virtual	~DriveOwner (void)
void	Set (const DriveCaller *pDC)
DriveCaller *	pGetDriveCaller (void) const
doublereal	dGet (const doublereal &dVar) const
doublereal	dGet (void) const
bool	bIsDifferentiable (void) const
doublereal	dGetP (const doublereal &dVar) const
doublereal	dGetP (void) const
Public Member Functions inherited from AerodynamicOutput
	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 Member Functions
virtual void	SetOutputFlag (flag f=flag(1))
void	Output_int (OutputHandler &OH) const
void	AddForce_int (const StructNode *pN, const Vec3 &F, const Vec3 &M, const Vec3 &X) const
void	AddSectionalForce_int (unsigned uPnt, const Vec3 &F, const Vec3 &M, doublereal dW, const Vec3 &X, const Mat3x3 &R, const Vec3 &V, const Vec3 &W) const

Protected Attributes
AeroData *	aerodata
InducedVelocity *	pIndVel
bool	bPassiveInducedVelocity
const ShapeOwner	Chord
const ShapeOwner	ForcePoint
const ShapeOwner	VelocityPoint
const ShapeOwner	Twist
const ShapeOwner	TipLoss
GaussDataIterator	GDI
std::vector< outa_t >	OUTA
Mat3xN	vx
Mat3xN	wx
Mat3xN	fq
Mat3xN	cq
bool	bJacobian
Protected Attributes inherited from WithLabel
unsigned int	uLabel
std::string	sName
Protected Attributes inherited from ToBeOutput
flag	fOutput
Protected Attributes inherited from AirPropOwner
const AirProperties *	pAirProperties
Protected Attributes inherited from DriveOwner
DriveCaller *	pDriveCaller
Protected Attributes inherited from AerodynamicOutput
flag	m_eOutput
OrientationDescription	od
std::vector< Aero_output >	OutputData
std::vector< Aero_output > ::iterator	OutputIter

Additional Inherited Members
Public Types inherited from Elem
enum	Type {   UNKNOWN = -1, AIRPROPERTIES = 0, INDUCEDVELOCITY, AUTOMATICSTRUCTURAL,   GRAVITY, BODY, JOINT, JOINT_REGULARIZATION,   BEAM, PLATE, FORCE, INERTIA,   ELECTRICBULK, ELECTRIC, THERMAL, HYDRAULIC,   BULK, LOADABLE, DRIVEN, EXTERNAL,   AEROMODAL, AERODYNAMIC, GENEL, SOCKETSTREAM_OUTPUT,   RTAI_OUTPUT = SOCKETSTREAM_OUTPUT, LASTELEMTYPE }
Public Types inherited from SimulationEntity
typedef std::vector< Hint * >	Hints
Public Types inherited from ToBeOutput
enum	{ OUTPUT = 0x1U, OUTPUT_MASK = 0xFU, OUTPUT_PRIVATE = 0x10U, OUTPUT_PRIVATE_MASK = ~OUTPUT_MASK }
Public Types inherited from AerodynamicElem
enum	Type {   UNKNOWN = -1, INDUCEDVELOCITY = 0, AEROMODAL, AERODYNAMICBODY,   AERODYNAMICBEAM, AERODYNAMICEXTERNAL, AERODYNAMICEXTERNALMODAL, AERODYNAMICLOADABLE,   AIRCRAFTINSTRUMENTS, GENERICFORCE, LASTAEROTYPE }
Public Types inherited from AerodynamicOutput
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)) }

Detailed Description

template<unsigned iNN>
class Aerodynamic2DElem< iNN >

Definition at line 145 of file aeroelem.h.

Constructor & Destructor Documentation

template<unsigned iNN>

Aerodynamic2DElem< iNN >::Aerodynamic2DElem	(	unsigned int	uLabel,
		const DofOwner *	pDO,
		InducedVelocity *	pR,
		bool	bPassive,
		const Shape *	pC,
		const Shape *	pF,
		const Shape *	pV,
		const Shape *	pT,
		const Shape *	pTL,
		integer	iN,
		AeroData *	a,
		const DriveCaller *	pDC,
		bool	bUseJacobian,
		OrientationDescription	ood,
		flag	fOut
	)

Definition at line 162 of file aeroelem.cc.

References Aerodynamic2DElem< iNN >::aerodata, ASSERT, and DEBUGCOUTFNAME.

: Elem(uLabel, fOut),
AerodynamicElem(uLabel, pDO, fOut),
InitialAssemblyElem(uLabel, fOut),
DriveOwner(pDC),
AerodynamicOutput(fOut, iNN*iN, ood),
aerodata(a),
pIndVel(pR),
bPassiveInducedVelocity(bPassive),
Chord(pC),
ForcePoint(pF),
VelocityPoint(pV),
Twist(pT),
TipLoss(pTL),
GDI(iN),
OUTA(iNN*iN, outa_Zero),
bJacobian(bUseJacobian)
{
        DEBUGCOUTFNAME("Aerodynamic2DElem::Aerodynamic2DElem");

        ASSERT(iNN >= 1 && iNN <= 3);
        ASSERT(aerodata != 0);
}

template<unsigned iNN>

Aerodynamic2DElem< iNN >::~Aerodynamic2DElem ( void  )

virtual

Definition at line 197 of file aeroelem.cc.

References DEBUGCOUTFNAME, and SAFEDELETE.

{
        DEBUGCOUTFNAME("Aerodynamic2DElem::~Aerodynamic2DElem");

        SAFEDELETE(aerodata);
}

Member Function Documentation

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::AddForce_int ( const StructNode *  pN, const Vec3 &  F, const Vec3 &  M, const Vec3 &  X  ) const

protected

Definition at line 626 of file aeroelem.cc.

{
        if (pIndVel != 0 && !bPassiveInducedVelocity
                && !pIndVel->bSectionalForces())
        {
                pIndVel->AddForce(this, pN, F, M, X);
        }
}

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::AddSectionalForce_int ( unsigned  uPnt, const Vec3 &  F, const Vec3 &  M, doublereal  dW, const Vec3 &  X, const Mat3x3 &  R, const Vec3 &  V, const Vec3 &  W  ) const

protected

Definition at line 642 of file aeroelem.cc.

{
        if (pIndVel != 0 && !bPassiveInducedVelocity
                && pIndVel->bSectionalForces())
        {
                pIndVel->AddSectionalForce(GetElemType(), this, uPnt,
                        F, M, dW, X, R, V, W);
        }
}

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::AfterConvergence ( const VectorHandler &  X, const VectorHandler &  XP  )

virtual

Reimplemented from SimulationEntity.

Definition at line 402 of file aeroelem.cc.

References AeroData::BIELAWA, AeroData::HARRIS, MBDYN_EXCEPT_ARGS, and AeroData::STEADY.

{
        /* Memoria in caso di forze instazionarie */
        switch (aerodata->Unsteady()) {
        case AeroData::STEADY:
                break;

        case AeroData::HARRIS:
                throw ErrGeneric(MBDYN_EXCEPT_ARGS);

        case AeroData::BIELAWA:
                for (unsigned i = 0; i < iNN*GDI.iGetNum(); i++) {
                        aerodata->Update(i);
                }
                break;

        default:
                throw ErrGeneric(MBDYN_EXCEPT_ARGS);
        }

        for (unsigned i = 0; i < iNN*GDI.iGetNum(); i++) {
                aerodata->AfterConvergence(i, X, XP);
        }
}

template<unsigned iNN>

std::ostream & Aerodynamic2DElem< iNN >::DescribeDof ( std::ostream &  out, const char *  prefix = "", bool  bInitial = false  ) const

virtual

Reimplemented from Elem.

Definition at line 236 of file aeroelem.cc.

References ASSERT.

{
        ASSERT(bInitial == false);

        integer iFirstIndex = iGetFirstIndex();
        integer iNumDof = aerodata->iGetNumDof();

        for (unsigned b = 0; b < iNN; b++) {
                for (integer i = 0; i < GDI.iGetNum(); i++) {
                        out 
                                << prefix << iFirstIndex + 1 << "->" << iFirstIndex + iNumDof << ": "
                                "internal states at point #" << i << " of " << GDI.iGetNum() << ", "
                                "block #" << b << " of " << iNN << std::endl;

                        iFirstIndex += iNumDof;
                }
        }

        return out;
}

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::DescribeDof ( std::vector< std::string > &  desc, bool  bInitial = false, int  i = -1  ) const

virtual

Reimplemented from Elem.

Definition at line 267 of file aeroelem.cc.

References ASSERT, elemnames, and MBDYN_EXCEPT_ARGS.

{
        if (i < -1) {
                // error
                throw ErrGeneric(MBDYN_EXCEPT_ARGS);
        }

        ASSERT(bInitial == false);

        std::ostringstream os;
        os << elemnames[iNN - 1] << "(" << GetLabel() << ")";

        integer iNumDof = aerodata->iGetNumDof();
        if (i == -1) {
                integer iTotDof = iNumDof*GDI.iGetNum();
                desc.resize(iTotDof);

                std::string name(os.str());

                for (integer s = 0; s < iTotDof; s++) {
                        os.str(name);
                        os.seekp(0, std::ios_base::end);
                        os << ": internal state #" << s % iNumDof << " of " << iNumDof
                                << " at point #" << s/iNumDof << " of " << GDI.iGetNum() << ", "
                                "block #" << s/(iNumDof*GDI.iGetNum()) << " of " << iNN;
                        desc[s] = os.str();
                }

                return;
        }

        desc.resize(1);
        os << ": internal state #" << i % iNumDof << " of " << iNumDof
                << " at point #" << i/iNumDof << " of " << GDI.iGetNum() << ", "
                "block #" << i/(iNumDof*GDI.iGetNum()) << " of " << iNN;
        desc[0] = os.str();
}

template<unsigned iNN>

std::ostream & Aerodynamic2DElem< iNN >::DescribeEq ( std::ostream &  out, const char *  prefix = "", bool  bInitial = false  ) const

virtual

Reimplemented from Elem.

Definition at line 308 of file aeroelem.cc.

References ASSERT.

{
        ASSERT(bInitial == false);

        integer iFirstIndex = iGetFirstIndex();
        integer iNumDof = aerodata->iGetNumDof();

        for (unsigned b = 0; b < iNN; b++) {
                for (integer i = 0; i < GDI.iGetNum(); i++) {
                        out 
                                << prefix << iFirstIndex + 1 << "->" << iFirstIndex + iNumDof
                                << ": dynamics equations at point #" << i << " of " << GDI.iGetNum() << ", "
                                "block #" << b << " of " << iNN << std::endl;

                        iFirstIndex += iNumDof;
                }
        }

        return out;
}

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::DescribeEq ( std::vector< std::string > &  desc, bool  bInitial = false, int  i = -1  ) const

virtual

Reimplemented from Elem.

Definition at line 332 of file aeroelem.cc.

References ASSERT, elemnames, and MBDYN_EXCEPT_ARGS.

{
        if (i < -1) {
                // error
                throw ErrGeneric(MBDYN_EXCEPT_ARGS);
        }

        ASSERT(bInitial == false);

        std::ostringstream os;
        os << elemnames[iNN - 1] << "(" << GetLabel() << ")";

        integer iNumDof = aerodata->iGetNumDof();
        if (i == -1) {
                integer iTotDof = iNumDof*GDI.iGetNum();
                desc.resize(iTotDof);

                std::string name(os.str());

                for (integer s = 0; s < iTotDof; s++) {
                        os.str(name);
                        os.seekp(0, std::ios_base::end);
                        os << ": internal equation #" << s % iNumDof << " of " << iNumDof
                                << " at point #" << s/iNumDof << " of " << GDI.iGetNum() << ", "
                                "block " << s/(iNumDof*GDI.iGetNum()) << " of " << iNN;
                        desc[s] = os.str();
                }

                return;
        }

        desc.resize(1);
        os << ": internal equation #" << i % iNumDof << " of " << iNumDof
                << " at point #" << i/iNumDof << " of " << GDI.iGetNum() << ", "
                "block " << i/(iNumDof*GDI.iGetNum()) << " of " << iNN;
        desc[0] = os.str();
}

template<unsigned iNN>

DofOrder::Order Aerodynamic2DElem< iNN >::GetDofType ( unsigned int  i ) const

virtual

Reimplemented from Elem.

Definition at line 373 of file aeroelem.cc.

References ASSERT.

{
        ASSERT(aerodata->iGetNumDof() > 0);

        return aerodata->GetDofType(i % aerodata->iGetNumDof());
}

template<unsigned iNN>

virtual Elem::Type Aerodynamic2DElem< iNN >::GetElemType ( void  ) const

inlinevirtual

Implements Elem.

Definition at line 199 of file aeroelem.h.

                                                 {
                return Elem::AERODYNAMIC;
        };

template<unsigned iNN>

virtual unsigned int Aerodynamic2DElem< iNN >::iGetInitialNumDof ( void  ) const

inlinevirtual

Implements SubjectToInitialAssembly.

Definition at line 229 of file aeroelem.h.

                                                           {
                return 0;
        };

template<unsigned iNN>

unsigned int Aerodynamic2DElem< iNN >::iGetNumDof ( void  ) const

virtual

Reimplemented from Elem.

Definition at line 229 of file aeroelem.cc.

{
        return aerodata->iGetNumDof()*iNN*GDI.iGetNum();
}

template<unsigned iNN>

VariableSubMatrixHandler & Aerodynamic2DElem< iNN >::InitialAssJac ( VariableSubMatrixHandler &  WorkMat, const VectorHandler &    )

virtual

Implements SubjectToInitialAssembly.

Definition at line 441 of file aeroelem.cc.

References DEBUGCOUTFNAME, and VariableSubMatrixHandler::SetNullMatrix().

{
        DEBUGCOUTFNAME("Aerodynamic2DElem::InitialAssJac");
        WorkMat.SetNullMatrix();
        return WorkMat;
}

Here is the call graph for this function:

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::InitialWorkSpaceDim ( integer *  piNumRows, integer *  piNumCols  ) const

virtual

Implements SubjectToInitialAssembly.

Definition at line 432 of file aeroelem.cc.

{
        *piNumRows = 6*iNN;
        *piNumCols = 1;
}

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::Output_int ( OutputHandler &  OH ) const

protected

Definition at line 544 of file aeroelem.cc.

References OutputHandler::AERODYNAMIC, dRaDegr, EULER_123, EULER_313, EULER_321, OutputHandler::GetCurrentStep(), MatR2EulerAngles123(), MatR2EulerAngles313(), MatR2EulerAngles321(), ORIENTATION_MATRIX, ORIENTATION_VECTOR, Vec3::pGetVec(), OutputHandler::UseNetCDF(), and RotManip::VecRot().

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

{
#ifdef USE_NETCDF
        if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) {
                for (std::vector<AeroNetCDFOutput>::const_iterator i = NetCDFOutputData.begin();
                        i != NetCDFOutputData.end(); ++i)
                {
                        if (i->Var_X) {
                                i->Var_X->put_rec(i->X.pGetVec(), OH.GetCurrentStep());
                        }

                        if (i->Var_Phi) {
                                Vec3 E;
                                switch (od) {
                                case EULER_123:
                                        E = MatR2EulerAngles123(i->R)*dRaDegr;
                                        break;

                                case EULER_313:
                                        E = MatR2EulerAngles313(i->R)*dRaDegr;
                                        break;

                                case EULER_321:
                                        E = MatR2EulerAngles321(i->R)*dRaDegr;
                                        break;

                                case ORIENTATION_VECTOR:
                                        E = RotManip::VecRot(i->R);
                                        break;

                                case ORIENTATION_MATRIX:
                                        break;

                                default:
                                        /* impossible */
                                        break;
                                }

                                switch (od) {
                                case EULER_123:
                                case EULER_313:
                                case EULER_321:
                                case ORIENTATION_VECTOR:
                                        i->Var_Phi->put_rec(E.pGetVec(), OH.GetCurrentStep());
                                        break;

                                case ORIENTATION_MATRIX:
                                        i->Var_Phi->put_rec(i->R.pGetMat(), OH.GetCurrentStep());
                                        break;

                                default:
                                        /* impossible */
                                        break;
                                }
                        }

                        if (i->Var_V) {
                                i->Var_V->put_rec(i->V.pGetVec(), OH.GetCurrentStep());
                        }

                        if (i->Var_W) {
                                i->Var_W->put_rec(i->W.pGetVec(), OH.GetCurrentStep());
                        }

                        if (i->Var_F) {
                                i->Var_F->put_rec(i->F.pGetVec(), OH.GetCurrentStep());
                        }

                        if (i->Var_M) {
                                i->Var_M->put_rec(i->M.pGetVec(), OH.GetCurrentStep());
                        }
                }
        }
#endif /* USE_NETCDF */
}

Here is the call graph for this function:

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::OutputPrepare ( OutputHandler &  OH )

virtual

Reimplemented from ToBeOutput.

Definition at line 451 of file aeroelem.cc.

References OutputHandler::AERODYNAMIC, ASSERT, elemnames, OutputHandler::IsOpen(), OutputHandler::NETCDF, AerodynamicOutput::OUTPUT_GP_F, AerodynamicOutput::OUTPUT_GP_M, AerodynamicOutput::OUTPUT_GP_R, AerodynamicOutput::OUTPUT_GP_V, AerodynamicOutput::OUTPUT_GP_W, AerodynamicOutput::OUTPUT_GP_X, and OutputHandler::UseNetCDF().

{
        if (bToBeOutput()) {
#ifdef USE_NETCDF
                if (OH.UseNetCDF(OutputHandler::AERODYNAMIC)) {
                        ASSERT(OH.IsOpen(OutputHandler::NETCDF));

                        std::ostringstream os;
                        os << "elem.aerodynamic." << GetLabel();
                        (void)OH.CreateVar(os.str(), elemnames[iNN - 1]);

                        os << '.';
                        std::string name = os.str();

                        int totgp = iNN*GDI.iGetNum();
                        NetCDFOutputData.resize(totgp);

                        int j = 0;
                        for (std::vector<AeroNetCDFOutput>::iterator i = NetCDFOutputData.begin();
                                i != NetCDFOutputData.end(); ++i, ++j)
                        {
                                os.str("");
                                os << "Gauss point #" << j << "/" << totgp;
                                std::string gp(os.str());

                                unsigned uOutputFlags = (fToBeOutput() & OUTPUT_GP_ALL);

                                /* Add NetCDF (output) variables to the BinFile object
                                 * and save the NcVar* pointer returned from add_var
                                 * as handle for later write accesses.
                                 * Define also variable attributes */
                                i->Var_X = 0;
                                if (uOutputFlags & AerodynamicOutput::OUTPUT_GP_X) {
                                        os.str(name);
                                        os.seekp(0, std::ios_base::end);
                                        os << "X_" << j;
                                        i->Var_X = OH.CreateVar<Vec3>(os.str(), "m",
                                                gp + " global position vector (X, Y, Z)");
                                }

                                i->Var_Phi = 0;
                                if (uOutputFlags & AerodynamicOutput::OUTPUT_GP_R) {
                                        os.str("");
                                        os << "_" << j;
                                        i->Var_Phi = OH.CreateRotationVar(name, os.str(), od,
                                                gp + " global");
                                }

                                i->Var_V = 0;
                                if (uOutputFlags & AerodynamicOutput::OUTPUT_GP_V) {
                                        os.str(name);
                                        os.seekp(0, std::ios_base::end);
                                        os << "V_" << j;
                                        i->Var_V = OH.CreateVar<Vec3>(os.str(), "m/s",
                                                gp + " global frame (V_X, V_Y, V_Z)");
                                }

                                i->Var_W = 0;
                                if (uOutputFlags & AerodynamicOutput::OUTPUT_GP_W) {
                                        os.str(name);
                                        os.seekp(0, std::ios_base::end);
                                        os << "Omega_" << j;
                                        i->Var_W = OH.CreateVar<Vec3>(os.str(), "radian/s",
                                                gp + " global frame (Omega_X, Omega_Y, Omega_Z)");
                                }

                                i->Var_F = 0;
                                if (uOutputFlags & AerodynamicOutput::OUTPUT_GP_F) {
                                        os.str(name);
                                        os.seekp(0, std::ios_base::end);
                                        os << "F_" << j;
                                        i->Var_F = OH.CreateVar<Vec3>(os.str(), "N",
                                                gp + " force in local frame (F_X, F_Y, F_Z)");
                                }

                                i->Var_M = 0;
                                if (uOutputFlags & AerodynamicOutput::OUTPUT_GP_M) {
                                        os.str(name);
                                        os.seekp(0, std::ios_base::end);
                                        os << "M_" << j;
                                        i->Var_M = OH.CreateVar<Vec3>(os.str(), "Nm",
                                                gp + " force in local frame (M_X, M_Y, M_Z)");
                                }
                        }
                }
#endif // USE_NETCDF
        }
}

Here is the call graph for this function:

template<unsigned iNN>

virtual const InducedVelocity* Aerodynamic2DElem< iNN >::pGetInducedVelocity ( void  ) const

inlinevirtual

Reimplemented from AerodynamicElem.

Definition at line 242 of file aeroelem.h.

                                                                       {
                return pIndVel;
        };

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::SetOutputFlag ( flag  f = flag(1) )

protectedvirtual

Reimplemented from ToBeOutput.

Definition at line 211 of file aeroelem.cc.

References DEBUGCOUTFNAME, AerodynamicOutput::SetOutputFlag(), and ToBeOutput::SetOutputFlag().

{
        DEBUGCOUTFNAME("Aerodynamic2DElem::SetOutputFlag");
        ToBeOutput::SetOutputFlag(f);
        AerodynamicOutput::SetOutputFlag(f, iNN*GDI.iGetNum());
}

Here is the call graph for this function:

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::SetValue ( DataManager *  pDM, VectorHandler &  X, VectorHandler &  XP, SimulationEntity::Hints *  h = 0  )

virtual

Reimplemented from SimulationEntity.

Definition at line 382 of file aeroelem.cc.

{
        integer iNumDof = aerodata->iGetNumDof();
        if (iNumDof) {
                vx.Resize(6*iNN);
                wx.Resize(6*iNN);
                fq.Resize(iNumDof);
                cq.Resize(iNumDof);

                vx.Reset();
                wx.Reset();
                fq.Reset();
                cq.Reset();
        }
}

template<unsigned iNN>

void Aerodynamic2DElem< iNN >::WorkSpaceDim ( integer *  piNumRows, integer *  piNumCols  ) const

virtual

Implements Elem.

Definition at line 221 of file aeroelem.cc.

{
        *piNumRows = *piNumCols = iNN*6 + iGetNumDof();
}

Member Data Documentation

template<unsigned iNN>

AeroData* Aerodynamic2DElem< iNN >::aerodata

protected

Definition at line 153 of file aeroelem.h.

Referenced by Aerodynamic2DElem< iNN >::Aerodynamic2DElem().

template<unsigned iNN>

bool Aerodynamic2DElem< iNN >::bJacobian

protected

Definition at line 169 of file aeroelem.h.

template<unsigned iNN>

bool Aerodynamic2DElem< iNN >::bPassiveInducedVelocity

protected

Definition at line 155 of file aeroelem.h.

template<unsigned iNN>

const ShapeOwner Aerodynamic2DElem< iNN >::Chord

protected

Definition at line 157 of file aeroelem.h.

template<unsigned iNN>

Mat3xN Aerodynamic2DElem< iNN >::cq

protected

Definition at line 167 of file aeroelem.h.

template<unsigned iNN>

const ShapeOwner Aerodynamic2DElem< iNN >::ForcePoint

protected

Definition at line 158 of file aeroelem.h.

template<unsigned iNN>

Mat3xN Aerodynamic2DElem< iNN >::fq

protected

Definition at line 167 of file aeroelem.h.

template<unsigned iNN>

GaussDataIterator Aerodynamic2DElem< iNN >::GDI

protected

Definition at line 163 of file aeroelem.h.

template<unsigned iNN>

std::vector<outa_t> Aerodynamic2DElem< iNN >::OUTA

protected

Definition at line 164 of file aeroelem.h.

template<unsigned iNN>

InducedVelocity* Aerodynamic2DElem< iNN >::pIndVel

protected

Definition at line 154 of file aeroelem.h.

template<unsigned iNN>

const ShapeOwner Aerodynamic2DElem< iNN >::TipLoss

protected

Definition at line 161 of file aeroelem.h.

template<unsigned iNN>

const ShapeOwner Aerodynamic2DElem< iNN >::Twist

protected

Definition at line 160 of file aeroelem.h.

template<unsigned iNN>

const ShapeOwner Aerodynamic2DElem< iNN >::VelocityPoint

protected

Definition at line 159 of file aeroelem.h.

template<unsigned iNN>

Mat3xN Aerodynamic2DElem< iNN >::vx

protected

Definition at line 167 of file aeroelem.h.

template<unsigned iNN>

Mat3xN Aerodynamic2DElem< iNN >::wx

protected

Definition at line 167 of file aeroelem.h.

---

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

• aeroelem.h
• aeroelem.cc