#include <aerodata_impl.h>

Inheritance diagram for C81MultipleAeroData:

Collaboration diagram for C81MultipleAeroData:

Public Member Functions
	C81MultipleAeroData (int i_p, int i_dim, AeroData::UnsteadyModel u, std::vector< unsigned > &p, std::vector< doublereal > &ub, std::vector< const c81_data * > &d, DriveCaller *ptime=0)

	~C81MultipleAeroData (void)

std::ostream &	Restart (std::ostream &out) const

void	SetSectionData (const doublereal &abscissa, const doublereal &chord, const doublereal &forcepoint, const doublereal &velocitypoint, const doublereal &twist, const doublereal &omega=0.)

int	GetForces (int i, const doublereal W, doublereal TNG, outa_t &OUTA)

int	GetForcesJac (int i, const doublereal W, doublereal TNG, Mat6x6 &J, outa_t &OUTA)

Public Member Functions inherited from AeroData
	AeroData (int i_p, int i_dim, UnsteadyModel u=STEADY, DriveCaller *pt=0)

virtual	~AeroData (void)

std::ostream &	RestartUnsteady (std::ostream &out) const

virtual void	SetAirData (const doublereal &rho, const doublereal &c)

virtual unsigned int	iGetNumDof (void) const

virtual DofOrder::Order	GetDofType (unsigned int i) const

virtual void	AssRes (SubVectorHandler &WorkVec, doublereal dCoef, const VectorHandler &XCurr, const VectorHandler &XPrimeCurr, integer iFirstIndex, integer iFirstSubIndex, int i, const doublereal W, doublereal TNG, outa_t &OUTA)

virtual void	AssJac (FullSubMatrixHandler &WorkMat, doublereal dCoef, const VectorHandler &XCurr, const VectorHandler &XPrimeCurr, integer iFirstIndex, integer iFirstSubIndex, const Mat3xN &vx, const Mat3xN &wx, Mat3xN &fq, Mat3xN &cq, int i, const doublereal W, doublereal TNG, Mat6x6 &J, outa_t &OUTA)

virtual void	AfterConvergence (int i, const VectorHandler &X, const VectorHandler &XP)

AeroData::UnsteadyModel	Unsteady (void) const

Public Member Functions inherited from AeroMemory
	AeroMemory (DriveCaller *pt)

virtual	~AeroMemory (void)

void	Predict (int i, doublereal alpha, doublereal &alf1, doublereal &alf2)

void	Update (int i)

void	SetNumPoints (int i)

int	GetNumPoints (void) const

Protected Attributes
std::vector< unsigned >	profiles

std::vector< doublereal >	upper_bounds

std::vector< const c81_data * >	data

integer	curr_data

Protected Attributes inherited from AeroData
UnsteadyModel	unsteadyflag

vam_t	VAM

doublereal	Omega

Protected Attributes inherited from AeroMemory
DriveCaller *	pTime

Additional Inherited Members
Public Types inherited from AeroData
enum	UnsteadyModel { STEADY = 0, HARRIS = 1, BIELAWA = 2, LAST }

enum	{ VX = 0, VY = 1, VZ = 2, WX = 3, WY = 4, WZ = 5, FX = 0, FY = 1, FZ = 2, MX = 3, MY = 4, MZ = 5 }

Protected Member Functions inherited from AeroData
int	StorageSize (void) const

int	GetForcesJacForwardDiff_int (int i, const doublereal W, doublereal TNG, Mat6x6 &J, outa_t &OUTA)

int	GetForcesJacCenteredDiff_int (int i, const doublereal W, doublereal TNG, Mat6x6 &J, outa_t &OUTA)

Detailed Description

Definition at line 88 of file aerodata_impl.h.

Constructor & Destructor Documentation

C81MultipleAeroData::C81MultipleAeroData	(	int	i_p,
		int	i_dim,
		AeroData::UnsteadyModel	u,
		std::vector< unsigned > &	p,
		std::vector< doublereal > &	ub,
		std::vector< const c81_data * > &	d,
		DriveCaller *	ptime = `0`
	)

Definition at line 157 of file aerodata_impl.cc.

References ASSERT, data, profiles, and upper_bounds.

 : AeroData(i_p, i_dim, u, ptime),
 profiles(p), upper_bounds(ub), data(d)
 {
         ASSERT(!profiles.empty());
         ASSERT(!upper_bounds.empty());
         ASSERT(!data.empty());
         ASSERT(profiles.size() == upper_bounds.size());
         ASSERT(profiles.size() == data.size());
 }

C81MultipleAeroData::~C81MultipleAeroData ( void )

Definition at line 174 of file aerodata_impl.cc.

References NO_OP.

 {
         NO_OP;
 }

Member Function Documentation

int C81MultipleAeroData::GetForces	(	int	i,
		const doublereal *	W,
		doublereal *	TNG,
		outa_t &	OUTA
	)

virtual

Reimplemented from AeroData.

Definition at line 215 of file aerodata_impl.cc.

References outa_t::alf1, outa_t::alf2, ASSERT, grad::atan2(), AeroData::BIELAWA, c81_aerod2_u(), curr_data, data, AeroData::HARRIS, AeroMemory::Predict(), AeroData::unsteadyflag, AeroData::VAM, AeroData::VX, and AeroData::VY.

 {
         switch (unsteadyflag) {
         case AeroData::HARRIS:
         case AeroData::BIELAWA:
                 Predict(i, atan2(-W[VY], W[VX]), OUTA.alf1, OUTA.alf2);
                 break;
 
         default:
                 break;
         }
 
         ASSERT(i >= 0);
         ASSERT(unsigned(i) < data.size());
 
         return c81_aerod2_u(const_cast<doublereal *>(W), &VAM, TNG, &OUTA,
                 const_cast<c81_data *>(data[curr_data]), unsteadyflag);
 }

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int C81MultipleAeroData::GetForcesJac	(	int	i,
		const doublereal *	W,
		doublereal *	TNG,
		Mat6x6 &	J,
		outa_t &	OUTA
	)

virtual

Reimplemented from AeroData.

Definition at line 235 of file aerodata_impl.cc.

References AeroData::GetForcesJacForwardDiff_int().

 {
         return AeroData::GetForcesJacForwardDiff_int(i, W, TNG, J, OUTA);
 }

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std::ostream & C81MultipleAeroData::Restart ( std::ostream & out ) const

virtual

Implements AeroData.

Definition at line 180 of file aerodata_impl.cc.

References profiles, AeroData::RestartUnsteady(), and upper_bounds.

 {
         out << "C81, multiple";
         for (unsigned i = 0; i < profiles.size(); i++) {
                 out << ", " << profiles[i] << ", " << upper_bounds[i];
         }
 
         return RestartUnsteady(out);
 }

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void C81MultipleAeroData::SetSectionData	(	const doublereal &	abscissa,
		const doublereal &	chord,
		const doublereal &	forcepoint,
		const doublereal &	velocitypoint,
		const doublereal &	twist,
		const doublereal &	omega = `0.`
	)

virtual

Reimplemented from AeroData.

Definition at line 191 of file aerodata_impl.cc.

References ASSERT, curr_data, profiles, AeroData::SetSectionData(), and upper_bounds.

 {
         ASSERT(abscissa >= -1. && abscissa <= 1.);
 
         AeroData::SetSectionData(abscissa, chord, forcepoint, velocitypoint,
                 twist, omega);
 
         for (int i = profiles.size() - 1; i--; ) {
                 if (abscissa > upper_bounds[i]) {
                         curr_data = i + 1;
                         return;
                 }
         }
 
         curr_data = 0;
 }