#include <EulerCFE.h>

Inheritance diagram for Nektar::EulerCFE:

Collaboration diagram for Nektar::EulerCFE:

Public Member Functions
virtual	~EulerCFE ()
	problem type selector More...

Public Member Functions inherited from Nektar::CompressibleFlowSystem
virtual	~CompressibleFlowSystem ()
	Destructor for CompressibleFlowSystem class. More...

NekDouble	GetStabilityLimit (int n)
	Function to calculate the stability limit for DG/CG. More...

Array< OneD, NekDouble >	GetStabilityLimitVector (const Array< OneD, int > &ExpOrder)
	Function to calculate the stability limit for DG/CG (a vector of them). More...

Public Member Functions inherited from Nektar::SolverUtils::UnsteadySystem
virtual SOLVER_UTILS_EXPORT	~UnsteadySystem ()
	Destructor. More...

SOLVER_UTILS_EXPORT NekDouble	GetTimeStep (const Array< OneD, const Array< OneD, NekDouble > > &inarray)
	Calculate the larger time-step mantaining the problem stable. More...

Public Member Functions inherited from Nektar::SolverUtils::EquationSystem
virtual SOLVER_UTILS_EXPORT	~EquationSystem ()
	Destructor. More...

SOLVER_UTILS_EXPORT void	SetUpTraceNormals (void)

SOLVER_UTILS_EXPORT void	InitObject ()
	Initialises the members of this object. More...

SOLVER_UTILS_EXPORT void	DoInitialise ()
	Perform any initialisation necessary before solving the problem. More...

SOLVER_UTILS_EXPORT void	DoSolve ()
	Solve the problem. More...

SOLVER_UTILS_EXPORT void	TransCoeffToPhys ()
	Transform from coefficient to physical space. More...

SOLVER_UTILS_EXPORT void	TransPhysToCoeff ()
	Transform from physical to coefficient space. More...

SOLVER_UTILS_EXPORT void	Output ()
	Perform output operations after solve. More...

SOLVER_UTILS_EXPORT NekDouble	LinfError (unsigned int field, const Array< OneD, NekDouble > &exactsoln=NullNekDouble1DArray)
	Linf error computation. More...

SOLVER_UTILS_EXPORT std::string	GetSessionName ()
	Get Session name. More...

template<class T >
boost::shared_ptr< T >	as ()

SOLVER_UTILS_EXPORT void	ResetSessionName (std::string newname)
	Reset Session name. More...

SOLVER_UTILS_EXPORT LibUtilities::SessionReaderSharedPtr	GetSession ()
	Get Session name. More...

SOLVER_UTILS_EXPORT MultiRegions::ExpListSharedPtr	GetPressure ()
	Get pressure field if available. More...

SOLVER_UTILS_EXPORT void	PrintSummary (std::ostream &out)
	Print a summary of parameters and solver characteristics. More...

SOLVER_UTILS_EXPORT void	SetLambda (NekDouble lambda)
	Set parameter m_lambda. More...

SOLVER_UTILS_EXPORT void	EvaluateFunction (Array< OneD, Array< OneD, NekDouble > > &pArray, std::string pFunctionName, const NekDouble pTime=0.0, const int domain=0)
	Evaluates a function as specified in the session file. More...

SOLVER_UTILS_EXPORT void	EvaluateFunction (std::vector< std::string > pFieldNames, Array< OneD, Array< OneD, NekDouble > > &pFields, const std::string &pName, const NekDouble &pTime=0.0, const int domain=0)
	Populate given fields with the function from session. More...

SOLVER_UTILS_EXPORT void	EvaluateFunction (std::vector< std::string > pFieldNames, Array< OneD, MultiRegions::ExpListSharedPtr > &pFields, const std::string &pName, const NekDouble &pTime=0.0, const int domain=0)
	Populate given fields with the function from session. More...

SOLVER_UTILS_EXPORT void	EvaluateFunction (std::string pFieldName, Array< OneD, NekDouble > &pArray, const std::string &pFunctionName, const NekDouble &pTime=0.0, const int domain=0)

SOLVER_UTILS_EXPORT std::string	DescribeFunction (std::string pFieldName, const std::string &pFunctionName, const int domain)
	Provide a description of a function for a given field name. More...

SOLVER_UTILS_EXPORT void	InitialiseBaseFlow (Array< OneD, Array< OneD, NekDouble > > &base)
	Perform initialisation of the base flow. More...

SOLVER_UTILS_EXPORT void	SetInitialConditions (NekDouble initialtime=0.0, bool dumpInitialConditions=true, const int domain=0)
	Initialise the data in the dependent fields. More...

SOLVER_UTILS_EXPORT void	EvaluateExactSolution (int field, Array< OneD, NekDouble > &outfield, const NekDouble time)
	Evaluates an exact solution. More...

SOLVER_UTILS_EXPORT NekDouble	L2Error (unsigned int field, const Array< OneD, NekDouble > &exactsoln, bool Normalised=false)
	Compute the L2 error between fields and a given exact solution. More...

SOLVER_UTILS_EXPORT NekDouble	L2Error (unsigned int field, bool Normalised=false)
	Compute the L2 error of the fields. More...

SOLVER_UTILS_EXPORT Array < OneD, NekDouble >	ErrorExtraPoints (unsigned int field)
	Compute error (L2 and L_inf) over an larger set of quadrature points return [L2 Linf]. More...

SOLVER_UTILS_EXPORT void	WeakAdvectionGreensDivergenceForm (const Array< OneD, Array< OneD, NekDouble > > &F, Array< OneD, NekDouble > &outarray)
	Compute the inner product $(\nabla \phi \cdot F)$ . More...

SOLVER_UTILS_EXPORT void	WeakAdvectionDivergenceForm (const Array< OneD, Array< OneD, NekDouble > > &F, Array< OneD, NekDouble > &outarray)
	Compute the inner product $(\phi, \nabla \cdot F)$ . More...

SOLVER_UTILS_EXPORT void	WeakAdvectionNonConservativeForm (const Array< OneD, Array< OneD, NekDouble > > &V, const Array< OneD, const NekDouble > &u, Array< OneD, NekDouble > &outarray, bool UseContCoeffs=false)
	Compute the inner product $(\phi, V\cdot \nabla u)$ . More...

f SOLVER_UTILS_EXPORT void	AdvectionNonConservativeForm (const Array< OneD, Array< OneD, NekDouble > > &V, const Array< OneD, const NekDouble > &u, Array< OneD, NekDouble > &outarray, Array< OneD, NekDouble > &wk=NullNekDouble1DArray)
	Compute the non-conservative advection. More...

SOLVER_UTILS_EXPORT void	WeakDGAdvection (const Array< OneD, Array< OneD, NekDouble > > &InField, Array< OneD, Array< OneD, NekDouble > > &OutField, bool NumericalFluxIncludesNormal=true, bool InFieldIsInPhysSpace=false, int nvariables=0)
	Calculate the weak discontinuous Galerkin advection. More...

SOLVER_UTILS_EXPORT void	WeakDGDiffusion (const Array< OneD, Array< OneD, NekDouble > > &InField, Array< OneD, Array< OneD, NekDouble > > &OutField, bool NumericalFluxIncludesNormal=true, bool InFieldIsInPhysSpace=false)
	Calculate weak DG Diffusion in the LDG form. More...

SOLVER_UTILS_EXPORT void	Checkpoint_Output (const int n)
	Write checkpoint file of m_fields. More...

SOLVER_UTILS_EXPORT void	Checkpoint_Output (const int n, MultiRegions::ExpListSharedPtr &field, std::vector< Array< OneD, NekDouble > > &fieldcoeffs, std::vector< std::string > &variables)
	Write checkpoint file of custom data fields. More...

SOLVER_UTILS_EXPORT void	Checkpoint_BaseFlow (const int n)
	Write base flow file of m_fields. More...

SOLVER_UTILS_EXPORT void	WriteFld (const std::string &outname)
	Write field data to the given filename. More...

SOLVER_UTILS_EXPORT void	WriteFld (const std::string &outname, MultiRegions::ExpListSharedPtr &field, std::vector< Array< OneD, NekDouble > > &fieldcoeffs, std::vector< std::string > &variables)
	Write input fields to the given filename. More...

SOLVER_UTILS_EXPORT void	ImportFld (const std::string &infile, Array< OneD, MultiRegions::ExpListSharedPtr > &pFields)
	Input field data from the given file. More...

SOLVER_UTILS_EXPORT void	ImportFldToMultiDomains (const std::string &infile, Array< OneD, MultiRegions::ExpListSharedPtr > &pFields, const int ndomains)
	Input field data from the given file to multiple domains. More...

SOLVER_UTILS_EXPORT void	ImportFld (const std::string &infile, std::vector< std::string > &fieldStr, Array< OneD, Array< OneD, NekDouble > > &coeffs)
	Output a field. Input field data into array from the given file. More...

SOLVER_UTILS_EXPORT void	ImportFld (const std::string &infile, MultiRegions::ExpListSharedPtr &pField, std::string &pFieldName)
	Output a field. Input field data into ExpList from the given file. More...

SOLVER_UTILS_EXPORT void	ScanForHistoryPoints ()
	Builds map of which element holds each history point. More...

SOLVER_UTILS_EXPORT void	WriteHistoryData (std::ostream &out)
	Probe each history point and write to file. More...

SOLVER_UTILS_EXPORT void	SessionSummary (SummaryList &vSummary)
	Write out a session summary. More...

SOLVER_UTILS_EXPORT Array < OneD, MultiRegions::ExpListSharedPtr > &	UpdateFields ()

SOLVER_UTILS_EXPORT LibUtilities::FieldMetaDataMap &	UpdateFieldMetaDataMap ()
	Get hold of FieldInfoMap so it can be updated. More...

SOLVER_UTILS_EXPORT NekDouble	GetFinalTime ()
	Return final time. More...

SOLVER_UTILS_EXPORT int	GetNcoeffs ()

SOLVER_UTILS_EXPORT int	GetNcoeffs (const int eid)

SOLVER_UTILS_EXPORT int	GetNumExpModes ()

SOLVER_UTILS_EXPORT const Array< OneD, int >	GetNumExpModesPerExp ()

SOLVER_UTILS_EXPORT int	GetNvariables ()

SOLVER_UTILS_EXPORT const std::string	GetVariable (unsigned int i)

SOLVER_UTILS_EXPORT int	GetTraceTotPoints ()

SOLVER_UTILS_EXPORT int	GetTraceNpoints ()

SOLVER_UTILS_EXPORT int	GetExpSize ()

SOLVER_UTILS_EXPORT int	GetPhys_Offset (int n)

SOLVER_UTILS_EXPORT int	GetCoeff_Offset (int n)

SOLVER_UTILS_EXPORT int	GetTotPoints ()

SOLVER_UTILS_EXPORT int	GetTotPoints (int n)

SOLVER_UTILS_EXPORT int	GetNpoints ()

SOLVER_UTILS_EXPORT int	GetNumElmVelocity ()

SOLVER_UTILS_EXPORT int	GetSteps ()

SOLVER_UTILS_EXPORT NekDouble	GetTimeStep ()

SOLVER_UTILS_EXPORT void	CopyFromPhysField (const int i, Array< OneD, NekDouble > &output)

SOLVER_UTILS_EXPORT void	CopyToPhysField (const int i, Array< OneD, NekDouble > &output)

SOLVER_UTILS_EXPORT void	SetSteps (const int steps)

SOLVER_UTILS_EXPORT void	ZeroPhysFields ()

SOLVER_UTILS_EXPORT void	FwdTransFields ()

SOLVER_UTILS_EXPORT void	GetFluxVector (const int i, Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, NekDouble > > &flux)

SOLVER_UTILS_EXPORT void	GetFluxVector (const int i, Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, NekDouble > > &fluxX, Array< OneD, Array< OneD, NekDouble > > &fluxY)

SOLVER_UTILS_EXPORT void	GetFluxVector (const int i, const int j, Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, NekDouble > > &flux)

SOLVER_UTILS_EXPORT void	NumericalFlux (Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, NekDouble > > &numflux)

SOLVER_UTILS_EXPORT void	NumericalFlux (Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, NekDouble > > &numfluxX, Array< OneD, Array< OneD, NekDouble > > &numfluxY)

SOLVER_UTILS_EXPORT void	NumFluxforScalar (const Array< OneD, Array< OneD, NekDouble > > &ufield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &uflux)

SOLVER_UTILS_EXPORT void	NumFluxforVector (const Array< OneD, Array< OneD, NekDouble > > &ufield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &qfield, Array< OneD, Array< OneD, NekDouble > > &qflux)

SOLVER_UTILS_EXPORT void	SetModifiedBasis (const bool modbasis)

SOLVER_UTILS_EXPORT int	NoCaseStringCompare (const string &s1, const string &s2)
	Perform a case-insensitive string comparison. More...

SOLVER_UTILS_EXPORT int	GetCheckpointNumber ()

SOLVER_UTILS_EXPORT void	SetCheckpointNumber (int num)

SOLVER_UTILS_EXPORT int	GetCheckpointSteps ()

SOLVER_UTILS_EXPORT void	SetCheckpointSteps (int num)

SOLVER_UTILS_EXPORT void	SetTime (const NekDouble time)

SOLVER_UTILS_EXPORT void	SetInitialStep (const int step)

SOLVER_UTILS_EXPORT void	SetBoundaryConditions (NekDouble time)
	Evaluates the boundary conditions at the given time. More...

virtual SOLVER_UTILS_EXPORT bool	v_NegatedOp ()
	Virtual function to identify if operator is negated in DoSolve. More...

Static Public Member Functions
static SolverUtils::EquationSystemSharedPtr	create (const LibUtilities::SessionReaderSharedPtr &pSession)
	Creates an instance of this class. More...

Static Public Member Functions inherited from Nektar::CompressibleFlowSystem
static SolverUtils::EquationSystemSharedPtr	create (const LibUtilities::SessionReaderSharedPtr &pSession)
	Creates an instance of this class. More...

Public Attributes
ProblemType	m_problemType

Public Attributes inherited from Nektar::SolverUtils::UnsteadySystem
NekDouble	m_cflSafetyFactor
	CFL safety factor (comprise between 0 to 1). More...

Static Public Attributes
static std::string	className
	Name of class. More...

Static Public Attributes inherited from Nektar::CompressibleFlowSystem
static std::string	className
	Name of class. More...

Protected Member Functions
	EulerCFE (const LibUtilities::SessionReaderSharedPtr &pSession)

virtual void	v_InitObject ()
	Initialization object for CompressibleFlowSystem class. More...

virtual void	v_GenerateSummary (SolverUtils::SummaryList &s)
	Print a summary of time stepping parameters. More...

void	DoOdeRhs (const Array< OneD, const Array< OneD, NekDouble > > &inarray, Array< OneD, Array< OneD, NekDouble > > &outarray, const NekDouble time)
	Compute the right-hand side. More...

void	DoOdeProjection (const Array< OneD, const Array< OneD, NekDouble > > &inarray, Array< OneD, Array< OneD, NekDouble > > &outarray, const NekDouble time)
	Compute the projection and call the method for imposing the boundary conditions in case of discontinuous projection. More...

virtual void	v_SetInitialConditions (NekDouble initialtime=0.0, bool dumpInitialConditions=true, const int domain=0)
	Set the initial conditions. More...

virtual void	v_EvaluateExactSolution (unsigned int field, Array< OneD, NekDouble > &outfield, const NekDouble time=0.0)
	Get the exact solutions for isentropic vortex and Ringleb flow problems. More...

Protected Member Functions inherited from Nektar::CompressibleFlowSystem
	CompressibleFlowSystem (const LibUtilities::SessionReaderSharedPtr &pSession)

void	GetFluxVector (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &flux)
	Return the flux vector for the compressible Euler equations. More...

void	GetFluxVectorDeAlias (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &flux)
	Return the flux vector for the compressible Euler equations by using the de-aliasing technique. More...

void	GetViscousFluxVector (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &derivatives, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &viscousTensor)
	Return the flux vector for the LDG diffusion problem. More...

void	GetFluxVectorPDESC (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &flux)

void	GetViscousFluxVectorDeAlias (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &derivatives, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &viscousTensor)
	Return the flux vector for the LDG diffusion problem. More...

void	SetCommonBC (const std::string &userDefStr, const int n, const NekDouble time, int &cnt, Array< OneD, Array< OneD, NekDouble > > &inarray)
	Set boundary conditions which can be: a) Wall and Symmerty BCs implemented at CompressibleFlowSystem level since they are compressible solver specific; b) Time dependent BCs. More...

void	WallBC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Wall boundary conditions for compressible flow problems. More...

void	WallViscousBC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Wall boundary conditions for viscous compressible flow problems. More...

void	SymmetryBC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Symmetry boundary conditions for compressible flow problems. More...

void	RiemannInvariantBC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Outflow characteristic boundary conditions for compressible flow problems. More...

void	PressureOutflowNonReflectiveBC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Pressure outflow non-reflective boundary conditions for compressible flow problems. More...

void	PressureOutflowBC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Pressure outflow boundary conditions for compressible flow problems. More...

void	PressureOutflowFileBC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Pressure outflow boundary conditions for compressible flow problems. More...

void	PressureInflowFileBC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Pressure inflow boundary conditions for compressible flow problems where either the density and the velocities are assigned from a file or the full state is assigned from a file (depending on the problem type, either subsonic or supersonic). More...

void	ExtrapOrder0BC (int bcRegion, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Extrapolation of order 0 for all the variables such that, at the boundaries, a trivial Riemann problem is solved. More...

void	GetVelocityVector (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, NekDouble > > &velocity)

void	GetSoundSpeed (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, NekDouble > &pressure, Array< OneD, NekDouble > &soundspeed)

void	GetMach (Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, NekDouble > &soundspeed, Array< OneD, NekDouble > &mach)

void	GetTemperature (const Array< OneD, const Array< OneD, NekDouble > > &physfield, Array< OneD, NekDouble > &pressure, Array< OneD, NekDouble > &temperature)

void	GetPressure (const Array< OneD, const Array< OneD, NekDouble > > &physfield, Array< OneD, NekDouble > &pressure)
	Calculate the pressure field $p = (\gamma-1)(E-\frac{1}{2}\rho\\| \mathbf{v} \\|^2)$ assuming an ideal gas law. More...

void	GetPressure (const Array< OneD, const Array< OneD, NekDouble > > &physfield, const Array< OneD, const Array< OneD, NekDouble > > &velocity, Array< OneD, NekDouble > &pressure)

void	GetEnthalpy (const Array< OneD, const Array< OneD, NekDouble > > &physfield, Array< OneD, NekDouble > &pressure, Array< OneD, NekDouble > &enthalpy)

void	GetEntropy (const Array< OneD, const Array< OneD, NekDouble > > &physfield, const Array< OneD, const NekDouble > &pressure, const Array< OneD, const NekDouble > &temperature, Array< OneD, NekDouble > &entropy)

void	GetSmoothArtificialViscosity (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, NekDouble > &eps_bar)

void	GetDynamicViscosity (const Array< OneD, const NekDouble > &temperature, Array< OneD, NekDouble > &mu)

void	GetStdVelocity (const Array< OneD, const Array< OneD, NekDouble > > &inarray, Array< OneD, NekDouble > &stdV)

virtual bool	v_PostIntegrate (int step)

bool	CalcSteadyState (bool output)

void	GetSensor (const Array< OneD, const Array< OneD, NekDouble > > &physarray, Array< OneD, NekDouble > &Sensor, Array< OneD, NekDouble > &SensorKappa)

void	GetElementDimensions (Array< OneD, Array< OneD, NekDouble > > &outarray, Array< OneD, NekDouble > &hmin)

void	GetAbsoluteVelocity (const Array< OneD, const Array< OneD, NekDouble > > &inarray, Array< OneD, NekDouble > &Vtot)

void	GetArtificialDynamicViscosity (const Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, NekDouble > &mu_var)

void	SetVarPOrderElmt (const Array< OneD, const Array< OneD, NekDouble > > &physfield, Array< OneD, NekDouble > &PolyOrder)

void	GetForcingTerm (const Array< OneD, const Array< OneD, NekDouble > > &inarray, Array< OneD, Array< OneD, NekDouble > > outarrayForcing)

virtual NekDouble	v_GetTimeStep (const Array< OneD, const Array< OneD, NekDouble > > &inarray)
	Return the timestep to be used for the next step in the time-marching loop. More...

NekDouble	GetGasConstant ()

NekDouble	GetGamma ()

const Array< OneD, const Array < OneD, NekDouble > > &	GetVecLocs ()

const Array< OneD, const Array < OneD, NekDouble > > &	GetNormals ()

virtual void	v_ExtraFldOutput (std::vector< Array< OneD, NekDouble > > &fieldcoeffs, std::vector< std::string > &variables)

Protected Member Functions inherited from Nektar::SolverUtils::UnsteadySystem
SOLVER_UTILS_EXPORT	UnsteadySystem (const LibUtilities::SessionReaderSharedPtr &pSession)
	Initialises UnsteadySystem class members. More...

SOLVER_UTILS_EXPORT NekDouble	MaxTimeStepEstimator ()
	Get the maximum timestep estimator for cfl control. More...

virtual SOLVER_UTILS_EXPORT void	v_DoSolve ()
	Solves an unsteady problem. More...

virtual SOLVER_UTILS_EXPORT void	v_DoInitialise ()
	Sets up initial conditions. More...

virtual SOLVER_UTILS_EXPORT void	v_AppendOutput1D (Array< OneD, Array< OneD, NekDouble > > &solution1D)
	Print the solution at each solution point in a txt file. More...

virtual SOLVER_UTILS_EXPORT void	v_NumericalFlux (Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, NekDouble > > &numflux)

virtual SOLVER_UTILS_EXPORT void	v_NumericalFlux (Array< OneD, Array< OneD, NekDouble > > &physfield, Array< OneD, Array< OneD, NekDouble > > &numfluxX, Array< OneD, Array< OneD, NekDouble > > &numfluxY)

virtual SOLVER_UTILS_EXPORT void	v_NumFluxforScalar (const Array< OneD, Array< OneD, NekDouble > > &ufield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &uflux)

virtual SOLVER_UTILS_EXPORT void	v_NumFluxforVector (const Array< OneD, Array< OneD, NekDouble > > &ufield, Array< OneD, Array< OneD, Array< OneD, NekDouble > > > &qfield, Array< OneD, Array< OneD, NekDouble > > &qflux)

virtual SOLVER_UTILS_EXPORT bool	v_PreIntegrate (int step)

virtual SOLVER_UTILS_EXPORT bool	v_SteadyStateCheck (int step)

SOLVER_UTILS_EXPORT void	CheckForRestartTime (NekDouble &time)

SOLVER_UTILS_EXPORT void	SVVVarDiffCoeff (const Array< OneD, Array< OneD, NekDouble > > vel, StdRegions::VarCoeffMap &varCoeffMap)
	Evaluate the SVV diffusion coefficient according to Moura's paper where it should proportional to h time velocity. More...

Protected Member Functions inherited from Nektar::SolverUtils::EquationSystem
SOLVER_UTILS_EXPORT	EquationSystem (const LibUtilities::SessionReaderSharedPtr &pSession)
	Initialises EquationSystem class members. More...

int	nocase_cmp (const string &s1, const string &s2)

virtual SOLVER_UTILS_EXPORT NekDouble	v_LinfError (unsigned int field, const Array< OneD, NekDouble > &exactsoln=NullNekDouble1DArray)
	Virtual function for the L_inf error computation between fields and a given exact solution. More...

virtual SOLVER_UTILS_EXPORT NekDouble	v_L2Error (unsigned int field, const Array< OneD, NekDouble > &exactsoln=NullNekDouble1DArray, bool Normalised=false)
	Virtual function for the L_2 error computation between fields and a given exact solution. More...

virtual SOLVER_UTILS_EXPORT void	v_TransCoeffToPhys ()
	Virtual function for transformation to physical space. More...

virtual SOLVER_UTILS_EXPORT void	v_TransPhysToCoeff ()
	Virtual function for transformation to coefficient space. More...

SOLVER_UTILS_EXPORT void	SetUpBaseFields (SpatialDomains::MeshGraphSharedPtr &mesh)

SOLVER_UTILS_EXPORT void	ImportFldBase (std::string pInfile, SpatialDomains::MeshGraphSharedPtr pGraph)

virtual SOLVER_UTILS_EXPORT void	v_Output (void)

virtual SOLVER_UTILS_EXPORT MultiRegions::ExpListSharedPtr	v_GetPressure (void)

Private Member Functions
void	SetBoundaryConditions (Array< OneD, Array< OneD, NekDouble > > &physarray, NekDouble time)
	Set boundary conditions which can be: a) Wall and Symmerty BCs implemented at CompressibleFlowSystem level since they are compressible solver specific; b) Isentropic vortex and Ringleb flow BCs implemented at EulerCFE level since they are Euler solver specific; c) Time dependent BCs. More...

void	EvaluateIsentropicVortex (const Array< OneD, NekDouble > &x, const Array< OneD, NekDouble > &y, const Array< OneD, NekDouble > &z, Array< OneD, Array< OneD, NekDouble > > &u, NekDouble time, const int o=0)
	Isentropic Vortex Test Case. More...

void	GetExactIsentropicVortex (int field, Array< OneD, NekDouble > &outarray, NekDouble time)
	Compute the exact solution for the isentropic vortex problem. More...

void	SetInitialIsentropicVortex (NekDouble initialtime)
	Set the initial condition for the isentropic vortex problem. More...

void	SetBoundaryIsentropicVortex (int bcRegion, NekDouble time, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Set the boundary conditions for the isentropic vortex problem. More...

void	GetExactRinglebFlow (int field, Array< OneD, NekDouble > &outarray)
	Ringleb Flow Test Case. More...

void	SetInitialRinglebFlow (void)
	Set the initial condition for the Ringleb flow problem. More...

void	SetBoundaryRinglebFlow (int bcRegion, NekDouble time, int cnt, Array< OneD, Array< OneD, NekDouble > > &physarray)
	Set the boundary conditions for the Ringleb flow problem. More...

Friends
class	MemoryManager< EulerCFE >

Additional Inherited Members
Protected Types inherited from Nektar::SolverUtils::EquationSystem
enum	HomogeneousType { eHomogeneous1D, eHomogeneous2D, eHomogeneous3D, eNotHomogeneous }
	Parameter for homogeneous expansions. More...

Protected Attributes inherited from Nektar::CompressibleFlowSystem
SolverUtils::RiemannSolverSharedPtr	m_riemannSolver

SolverUtils::RiemannSolverSharedPtr	m_riemannSolverLDG

SolverUtils::AdvectionSharedPtr	m_advection

SolverUtils::DiffusionSharedPtr	m_diffusion

Array< OneD, Array< OneD, NekDouble > >	m_vecLocs

NekDouble	m_gamma

NekDouble	m_pInf

NekDouble	m_rhoInf

NekDouble	m_uInf

NekDouble	m_vInf

NekDouble	m_wInf

NekDouble	m_UInf

NekDouble	m_gasConstant

NekDouble	m_Twall

std::string	m_ViscosityType

std::string	m_shockCaptureType

std::string	m_EqTypeStr

NekDouble	m_mu

NekDouble	m_Skappa

NekDouble	m_Kappa

NekDouble	m_mu0

NekDouble	m_FacL

NekDouble	m_FacH

NekDouble	m_eps_max

NekDouble	m_thermalConductivity

NekDouble	m_Cp

NekDouble	m_C1

NekDouble	m_C2

NekDouble	m_hFactor

NekDouble	m_Prandtl

NekDouble	m_amplitude

NekDouble	m_omega

std::ofstream	m_errFile

int	m_steadyStateSteps

NekDouble	m_steadyStateTol

std::vector < SolverUtils::ForcingSharedPtr >	m_forcing

StdRegions::StdQuadExpSharedPtr	m_OrthoQuadExp

StdRegions::StdHexExpSharedPtr	m_OrthoHexExp

bool	m_smoothDiffusion

Array< OneD, NekDouble >	m_pressureStorage

Array< OneD, Array< OneD, NekDouble > >	m_fieldStorage

Array< OneD, Array< OneD, NekDouble > >	m_un

Protected Attributes inherited from Nektar::SolverUtils::UnsteadySystem
int	m_infosteps
	Number of time steps between outputting status information. More...

LibUtilities::TimeIntegrationWrapperSharedPtr	m_intScheme
	Wrapper to the time integration scheme. More...

LibUtilities::TimeIntegrationSchemeOperators	m_ode
	The time integration scheme operators to use. More...

LibUtilities::TimeIntegrationSolutionSharedPtr	m_intSoln

NekDouble	m_epsilon

bool	m_explicitDiffusion
	Indicates if explicit or implicit treatment of diffusion is used. More...

bool	m_explicitAdvection
	Indicates if explicit or implicit treatment of advection is used. More...

bool	m_explicitReaction
	Indicates if explicit or implicit treatment of reaction is used. More...

bool	m_homoInitialFwd
	Flag to determine if simulation should start in homogeneous forward transformed state. More...

std::vector< int >	m_intVariables

std::vector< FilterSharedPtr >	m_filters

Protected Attributes inherited from Nektar::SolverUtils::EquationSystem
LibUtilities::CommSharedPtr	m_comm
	Communicator. More...

LibUtilities::SessionReaderSharedPtr	m_session
	The session reader. More...

LibUtilities::FieldIOSharedPtr	m_fld
	Field input/output. More...

map< std::string, Array< OneD, Array< OneD, float > > >	m_interpWeights
	Map of the interpolation weights for a specific filename. More...

map< std::string, Array< OneD, Array< OneD, unsigned int > > >	m_interpInds
	Map of the interpolation indices for a specific filename. More...

Array< OneD, MultiRegions::ExpListSharedPtr >	m_fields
	Array holding all dependent variables. More...

Array< OneD, MultiRegions::ExpListSharedPtr >	m_base
	Base fields. More...

Array< OneD, MultiRegions::ExpListSharedPtr >	m_derivedfields
	Array holding all dependent variables. More...

SpatialDomains::BoundaryConditionsSharedPtr	m_boundaryConditions
	Pointer to boundary conditions object. More...

SpatialDomains::MeshGraphSharedPtr	m_graph
	Pointer to graph defining mesh. More...

std::string	m_sessionName
	Name of the session. More...

NekDouble	m_time
	Current time of simulation. More...

int	m_initialStep
	Number of the step where the simulation should begin. More...

NekDouble	m_fintime
	Finish time of the simulation. More...

NekDouble	m_timestep
	Time step size. More...

NekDouble	m_lambda
	Lambda constant in real system if one required. More...

std::set< std::string >	m_loadedFields

NekDouble	m_checktime
	Time between checkpoints. More...

int	m_nchk
	Number of checkpoints written so far. More...

int	m_steps
	Number of steps to take. More...

int	m_checksteps
	Number of steps between checkpoints. More...

int	m_spacedim
	Spatial dimension (>= expansion dim). More...

int	m_expdim
	Expansion dimension. More...

bool	m_singleMode
	Flag to determine if single homogeneous mode is used. More...

bool	m_halfMode
	Flag to determine if half homogeneous mode is used. More...

bool	m_multipleModes
	Flag to determine if use multiple homogenenous modes are used. More...

bool	m_useFFT
	Flag to determine if FFT is used for homogeneous transform. More...

bool	m_homogen_dealiasing
	Flag to determine if dealiasing is used for homogeneous simulations. More...

bool	m_specHP_dealiasing
	Flag to determine if dealisising is usde for the Spectral/hp element discretisation. More...

enum MultiRegions::ProjectionType	m_projectionType
	Type of projection; e.g continuous or discontinuous. More...

Array< OneD, Array< OneD, NekDouble > >	m_traceNormals
	Array holding trace normals for DG simulations in the forwards direction. More...

Array< OneD, Array< OneD, Array< OneD, NekDouble > > >	m_gradtan
	1 x nvariable x nq More...

Array< OneD, Array< OneD, Array< OneD, NekDouble > > >	m_tanbasis
	2 x m_spacedim x nq More...

Array< OneD, bool >	m_checkIfSystemSingular
	Flag to indicate if the fields should be checked for singularity. More...

LibUtilities::FieldMetaDataMap	m_fieldMetaDataMap
	Map to identify relevant solver info to dump in output fields. More...

int	m_NumQuadPointsError
	Number of Quadrature points used to work out the error. More...

enum HomogeneousType	m_HomogeneousType

NekDouble	m_LhomX
	physical length in X direction (if homogeneous) More...

NekDouble	m_LhomY
	physical length in Y direction (if homogeneous) More...

NekDouble	m_LhomZ
	physical length in Z direction (if homogeneous) More...

int	m_npointsX
	number of points in X direction (if homogeneous) More...

int	m_npointsY
	number of points in Y direction (if homogeneous) More...

int	m_npointsZ
	number of points in Z direction (if homogeneous) More...

int	m_HomoDirec
	number of homogenous directions More...

int	m_NumMode
	Mode to use in case of single mode analysis. More...

Detailed Description

Definition at line 58 of file EulerCFE.h.

Constructor & Destructor Documentation

Nektar::EulerCFE::~EulerCFE ( )

virtual

problem type selector

Destructor for EulerCFE class.

Definition at line 95 of file EulerCFE.cpp.

96 {

97 }

Nektar::EulerCFE::EulerCFE ( const LibUtilities::SessionReaderSharedPtr & pSession )

protected

Definition at line 52 of file EulerCFE.cpp.

     : CompressibleFlowSystem(pSession)
     {
     }

Member Function Documentation

static SolverUtils::EquationSystemSharedPtr Nektar::EulerCFE::create ( const LibUtilities::SessionReaderSharedPtr & pSession )

inlinestatic

Creates an instance of this class.

Definition at line 64 of file EulerCFE.h.

References Nektar::MemoryManager< DataType >::AllocateSharedPtr().

         {
             SolverUtils::EquationSystemSharedPtr p = MemoryManager<EulerCFE>::AllocateSharedPtr(pSession);
             p->InitObject();
             return p;
         }

void Nektar::EulerCFE::DoOdeProjection	(	const Array< OneD, const Array< OneD, NekDouble > > &	inarray,
		Array< OneD, Array< OneD, NekDouble > > &	outarray,
		const NekDouble	time
	)

protected

Compute the projection and call the method for imposing the boundary conditions in case of discontinuous projection.

Definition at line 173 of file EulerCFE.cpp.

References ASSERTL0, Nektar::MultiRegions::eDiscontinuous, Nektar::MultiRegions::eGalerkin, Nektar::MultiRegions::eMixed_CG_Discontinuous, Nektar::SolverUtils::EquationSystem::GetNpoints(), Nektar::SolverUtils::EquationSystem::m_projectionType, SetBoundaryConditions(), and Vmath::Vcopy().

Referenced by v_InitObject().

     {
         int i;
         int nvariables = inarray.num_elements();
         
         switch (m_projectionType)
         {
             case MultiRegions::eDiscontinuous:
             {
                 // Just copy over array
                 int npoints = GetNpoints();
                 
                 for(i = 0; i < nvariables; ++i)
                 {
                     Vmath::Vcopy(npoints, inarray[i], 1, outarray[i], 1);
                 }
                 SetBoundaryConditions(outarray, time);
                 break;
             }
             case MultiRegions::eGalerkin:
             case MultiRegions::eMixed_CG_Discontinuous:
             {
                 ASSERTL0(false, "No Continuous Galerkin for Euler equations");
                 break;
             }
             default:
                 ASSERTL0(false, "Unknown projection scheme");
                 break;
         }
     }

void Nektar::EulerCFE::DoOdeRhs	(	const Array< OneD, const Array< OneD, NekDouble > > &	inarray,
		Array< OneD, Array< OneD, NekDouble > > &	outarray,
		const NekDouble	time
	)

protected

Compute the right-hand side.

Definition at line 142 of file EulerCFE.cpp.

References Nektar::SolverUtils::EquationSystem::GetNpoints(), Nektar::CompressibleFlowSystem::m_advection, Nektar::SolverUtils::EquationSystem::m_fields, Nektar::CompressibleFlowSystem::m_forcing, Nektar::SolverUtils::EquationSystem::m_spacedim, and Vmath::Neg().

Referenced by v_InitObject().

     {
         int i;
         int nvariables = inarray.num_elements();
         int npoints    = GetNpoints();
 
         Array<OneD, Array<OneD, NekDouble> > advVel(m_spacedim);
 
         m_advection->Advect(nvariables, m_fields, advVel, inarray,
                             outarray, time);
 
         for (i = 0; i < nvariables; ++i)
         {
             Vmath::Neg(npoints, outarray[i], 1);
         }
         
         // Add sponge layer if defined in the session file
         std::vector<SolverUtils::ForcingSharedPtr>::const_iterator x;
         for (x = m_forcing.begin(); x != m_forcing.end(); ++x)
         {
             (*x)->Apply(m_fields, inarray, outarray, time);
         }
     }

void Nektar::EulerCFE::EvaluateIsentropicVortex	(	const Array< OneD, NekDouble > &	x,
		const Array< OneD, NekDouble > &	y,
		const Array< OneD, NekDouble > &	z,
		Array< OneD, Array< OneD, NekDouble > > &	u,
		NekDouble	time,
		const int	o = `0`
	)

private

Isentropic Vortex Test Case.

Definition at line 288 of file EulerCFE.cpp.

References Nektar::CompressibleFlowSystem::m_gamma, Nektar::SolverUtils::EquationSystem::m_spacedim, and Vmath::Zero().

Referenced by GetExactIsentropicVortex(), SetBoundaryIsentropicVortex(), and SetInitialIsentropicVortex().

     {
         int nq = x.num_elements();
         
         // Flow parameters
         const NekDouble x0    = 5.0;
         const NekDouble y0    = 0.0;
         const NekDouble beta  = 5.0;
         const NekDouble u0    = 1.0;
         const NekDouble v0    = 0.5;
         const NekDouble gamma = m_gamma;
         NekDouble r, xbar, ybar, tmp;
         NekDouble fac = 1.0/(16.0*gamma*M_PI*M_PI);
         
         // In 3D zero rhow field.
         if (m_spacedim == 3)
         {
             Vmath::Zero(nq, &u[3][o], 1);
         }
         
         // Fill storage
         for (int i = 0; i < nq; ++i)
         {
             xbar      = x[i] - u0*time - x0;
             ybar      = y[i] - v0*time - y0;
             r         = sqrt(xbar*xbar + ybar*ybar);
             tmp       = beta*exp(1-r*r);
             u[0][i+o] = pow(1.0 - (gamma-1.0)*tmp*tmp*fac, 1.0/(gamma-1.0));
             u[1][i+o] = u[0][i+o]*(u0 - tmp*ybar/(2*M_PI));
             u[2][i+o] = u[0][i+o]*(v0 + tmp*xbar/(2*M_PI));
             u[m_spacedim+1][i+o] = pow(u[0][i+o], gamma)/(gamma-1.0) +
             0.5*(u[1][i+o]*u[1][i+o] + u[2][i+o]*u[2][i+o]) / u[0][i+o];
         }
     }

void Nektar::EulerCFE::GetExactIsentropicVortex	(	int	field,
		Array< OneD, NekDouble > &	outarray,
		NekDouble	time
	)

private

Compute the exact solution for the isentropic vortex problem.

Definition at line 332 of file EulerCFE.cpp.

References EvaluateIsentropicVortex(), Nektar::SolverUtils::EquationSystem::GetTotPoints(), Nektar::SolverUtils::EquationSystem::m_fields, Nektar::SolverUtils::EquationSystem::m_spacedim, and Vmath::Vcopy().

Referenced by v_EvaluateExactSolution().

     {
         int nTotQuadPoints  = GetTotPoints();
         Array<OneD, NekDouble> x(nTotQuadPoints);
         Array<OneD, NekDouble> y(nTotQuadPoints);
         Array<OneD, NekDouble> z(nTotQuadPoints);
         Array<OneD, Array<OneD, NekDouble> > u(m_spacedim+2);
         
         m_fields[0]->GetCoords(x, y, z);
         
         for (int i = 0; i < m_spacedim + 2; ++i)
         {
             u[i] = Array<OneD, NekDouble>(nTotQuadPoints);
         }
         
         EvaluateIsentropicVortex(x, y, z, u, time);
         
         Vmath::Vcopy(nTotQuadPoints, u[field], 1, outarray, 1);
     }

void Nektar::EulerCFE::GetExactRinglebFlow	(	int	field,
		Array< OneD, NekDouble > &	outarray
	)

private

Ringleb Flow Test Case.

Compute the exact solution for the Ringleb flow problem.

Definition at line 438 of file EulerCFE.cpp.

References ASSERTL0, Nektar::SolverUtils::EquationSystem::GetTotPoints(), Nektar::SolverUtils::EquationSystem::m_fields, and Nektar::CompressibleFlowSystem::m_gamma.

Referenced by v_EvaluateExactSolution().

     {
         int nTotQuadPoints  = GetTotPoints();
         
         Array<OneD, NekDouble> rho(nTotQuadPoints, 100.0);
         Array<OneD, NekDouble> rhou(nTotQuadPoints);
         Array<OneD, NekDouble> rhov(nTotQuadPoints);
         Array<OneD, NekDouble> E(nTotQuadPoints);
         Array<OneD, NekDouble> x(nTotQuadPoints);
         Array<OneD, NekDouble> y(nTotQuadPoints);
         Array<OneD, NekDouble> z(nTotQuadPoints);
         
         m_fields[0]->GetCoords(x, y, z);
         
         // Flow parameters
         NekDouble c, k, phi, r, J, VV, pp, sint, P, ss;
         NekDouble J11, J12, J21, J22, det;
         NekDouble Fx, Fy;
         NekDouble xi, yi;
         NekDouble dV;
         NekDouble dtheta;
         NekDouble par1;
         NekDouble theta     = M_PI / 4.0;
         NekDouble kExt      = 0.7;
         NekDouble V         = kExt * sin(theta);
         NekDouble toll      = 1.0e-8;
         NekDouble errV      = 1.0;
         NekDouble errTheta  = 1.0;
         NekDouble gamma     = m_gamma;
         NekDouble gamma_1_2 = (gamma - 1.0) / 2.0;
         
         for (int i = 0; i < nTotQuadPoints; ++i)
         {
             while ((abs(errV) > toll) || (abs(errTheta) > toll))
             {
                 VV   = V * V;
                 sint = sin(theta);
                 c    = sqrt(1.0 - gamma_1_2 * VV);
                 k    = V / sint;
                 phi  = 1.0 / k;
                 pp   = phi * phi;
                 J    = 1.0 / c + 1.0 / (3.0 * c * c * c) + 
                 1.0 / (5.0 * c * c * c * c * c) - 
                 0.5 * log((1.0 + c) / (1.0 - c));
                 
                 r    = pow(c, 1.0 / gamma_1_2);
                 xi   = 1.0 / (2.0 * r) * (1.0 / VV - 2.0 * pp) + J / 2.0;
                 yi   = phi / (r * V) * sqrt(1.0 - VV * pp);
                 par1 = 25.0 - 5.0 * VV;
                 ss   = sint * sint;
                 
                 Fx   = xi - x[i];
                 Fy   = yi - y[i];
                 
                 J11  = 39062.5 / pow(par1, 3.5) * (1.0 / VV - 2.0 / VV * ss) * 
                 V + 1562.5 / pow(par1, 2.5) * (-2.0 / (VV * V) + 4.0 / 
                 (VV * V) * ss) + 12.5 / pow(par1, 1.5) * V + 312.5 / 
                 pow(par1, 2.5) * V + 7812.5 / pow(par1, 3.5) * V - 
                 0.25 * (-1.0 / pow(par1, 0.5) * V/(1.0 - 0.2 * 
                 pow(par1, 0.5)) - (1.0 + 0.2 * pow(par1, 0.5)) / 
                 pow((1.0 - 0.2 * pow(par1, 0.5)), 2.0) / 
                 pow(par1, 0.5) * V) / (1.0 + 0.2 * pow(par1, 0.5)) * 
                 (1.0 - 0.2 * pow(par1, 0.5));
                 
                 J12  = -6250.0 / pow(par1, 2.5) / VV * sint * cos(theta);
                 J21  = -6250.0 / (VV * V) * sint / 
                 pow(par1, 2.5) * pow((1.0 - ss), 0.5) + 
                 78125.0 / V * sint / pow(par1, 3.5) * 
                 pow((1.0 - ss), 0.5);
                 
                 // the matrix is singular when theta = pi/2
                 if(abs(y[i])<toll && abs(cos(theta))<toll)
                 {
                     J22 = -39062.5 / pow(par1, 3.5) / V + 3125 / 
                     pow(par1, 2.5) / (VV * V) + 12.5 / pow(par1, 1.5) * 
                     V + 312.5 / pow(par1, 2.5) * V + 7812.5 / 
                     pow(par1, 3.5) * V - 0.25 * (-1.0 / pow(par1, 0.5) *
                     V / (1.0 - 0.2 * pow(par1, 0.5)) - (1.0 + 0.2 * 
                     pow(par1, 0.5)) / pow((1.0 - 0.2 * 
                     pow(par1, 0.5)), 2.0) / pow(par1, 0.5) * V) / 
                     (1.0 + 0.2 * pow(par1, 0.5)) * (1.0 - 0.2 * 
                     pow(par1,0.5));
                     
                     // dV = -dV/dx * Fx
                     dV      = -1.0 / J22 * Fx;
                     dtheta  = 0.0;
                     theta   = M_PI / 2.0;
                 }
                 else
                 {
                     J22 = 3125.0 / VV * cos(theta) / pow(par1, 2.5) * 
                     pow((1.0 - ss), 0.5) - 3125.0 / VV * ss / 
                     pow(par1, 2.5) / pow((1.0 - ss), 0.5) * cos(theta);
                     
                     det = -1.0 / (J11 * J22 - J12 * J21);
                     
                     // [dV dtheta]' = -[invJ]*[Fx Fy]'
                     dV     = det * ( J22 * Fx - J12 * Fy);
                     dtheta = det * (-J21 * Fx + J11 * Fy);
                 }
                 
                 V     = V + dV;
                 theta = theta + dtheta;
                 
                 errV     = abs(dV);
                 errTheta = abs(dtheta);
                 
             }
             
             c = sqrt(1.0 - gamma_1_2 * VV);
             r = pow(c, 1.0 / gamma_1_2);
             
             rho[i]  = r;
             rhou[i] = rho[i] * V * cos(theta);
             rhov[i] = rho[i] * V * sin(theta);
             P       = (c * c) * rho[i] / gamma;
             E[i]    = P / (gamma - 1.0) + 0.5 * 
             (rhou[i] * rhou[i] / rho[i] + rhov[i] * rhov[i] / rho[i]);
             
             // Resetting the guess value
             errV     = 1.0;
             errTheta = 1.0;
             theta    = M_PI/4.0;
             V        = kExt*sin(theta);
         }
         
         switch (field)
         {
             case 0:
                 outarray = rho;
                 break;
             case 1:
                 outarray = rhou;
                 break;
             case 2:
                 outarray = rhov;
                 break;
             case 3:
                 outarray = E;
                 break;
             default:
                 ASSERTL0(false, "Error in variable number!");
                 break;
         }
     }

void Nektar::EulerCFE::SetBoundaryConditions	(	Array< OneD, Array< OneD, NekDouble > > &	inarray,
		NekDouble	time
	)

private

Set boundary conditions which can be: a) Wall and Symmerty BCs implemented at CompressibleFlowSystem level since they are compressible solver specific; b) Isentropic vortex and Ringleb flow BCs implemented at EulerCFE level since they are Euler solver specific; c) Time dependent BCs.

Parameters

inarray	fields array.
time	time.

Definition at line 218 of file EulerCFE.cpp.

References ASSERTL0, Nektar::SolverUtils::EquationSystem::m_fields, SetBoundaryIsentropicVortex(), SetBoundaryRinglebFlow(), and Nektar::CompressibleFlowSystem::SetCommonBC().

Referenced by DoOdeProjection().

     {
         std::string varName;
         int cnt        = 0;
         
         std::string userDefStr;
         int nreg = m_fields[0]->GetBndConditions().num_elements();
         // Loop over Boundary Regions
         for (int n = 0; n < nreg; ++n)
         {
             userDefStr = m_fields[0]->GetBndConditions()[n]->GetUserDefined();
             if(!userDefStr.empty())
             {
                 if(boost::iequals(userDefStr,"WallViscous"))
                 {
                     ASSERTL0(false, "WallViscous is a wrong bc for the "
                              "Euler equations");
                 }
                 else if(boost::iequals(userDefStr, "IsentropicVortex"))
                 {
                     // Isentropic Vortex Boundary Condition
                     SetBoundaryIsentropicVortex(n, time, cnt, inarray);
                 }
                 else if (boost::iequals(userDefStr,"RinglebFlow"))
                 {
                     SetBoundaryRinglebFlow(n, time, cnt, inarray);
                 }
                 else
                 {
                     // set up userdefined BC common to all solvers
                     SetCommonBC(userDefStr,n,time, cnt,inarray);
                 }
             }
 
             // no User Defined conditions provided so skip cnt 
             cnt += m_fields[0]->GetBndCondExpansions()[n]->GetExpSize(); 
         }
     }

void Nektar::EulerCFE::SetBoundaryIsentropicVortex	(	int	bcRegion,
		NekDouble	time,
		int	cnt,
		Array< OneD, Array< OneD, NekDouble > > &	physarray
	)

private

Set the boundary conditions for the isentropic vortex problem.

Definition at line 388 of file EulerCFE.cpp.

References EvaluateIsentropicVortex(), Nektar::SolverUtils::EquationSystem::GetTraceTotPoints(), Nektar::SolverUtils::EquationSystem::m_fields, and Vmath::Vcopy().

Referenced by SetBoundaryConditions().

     {
         int nvariables      = physarray.num_elements();
         int nTraceNumPoints = GetTraceTotPoints();
         Array<OneD, Array<OneD, NekDouble> > Fwd(nvariables);
         const Array<OneD, const int> &bndTraceMap = m_fields[0]->GetTraceBndMap();
         
         // Get physical values of the forward trace (from exp to phys)
         for (int i = 0; i < nvariables; ++i)
         {
             Fwd[i] = Array<OneD, NekDouble>(nTraceNumPoints);
             m_fields[i]->ExtractTracePhys(physarray[i], Fwd[i]);
         }
         
         int id2, e_max;
         e_max = m_fields[0]->GetBndCondExpansions()[bcRegion]->GetExpSize();
         
         for(int e = 0; e < e_max; ++e)
         {
             int npoints = m_fields[0]->
             GetBndCondExpansions()[bcRegion]->GetExp(e)->GetTotPoints();
             int id1  = m_fields[0]->
             GetBndCondExpansions()[bcRegion]->GetPhys_Offset(e);
             id2 = m_fields[0]->GetTrace()->GetPhys_Offset(bndTraceMap[cnt++]);
             
             Array<OneD,NekDouble> x(npoints, 0.0);
             Array<OneD,NekDouble> y(npoints, 0.0);
             Array<OneD,NekDouble> z(npoints, 0.0);
             
             m_fields[0]->GetBndCondExpansions()[bcRegion]->
             GetExp(e)->GetCoords(x, y, z);
             
             EvaluateIsentropicVortex(x, y, z, Fwd, time, id2);
             
             for (int i = 0; i < nvariables; ++i)
             {
                 Vmath::Vcopy(npoints, &Fwd[i][id2], 1, 
                              &(m_fields[i]->GetBndCondExpansions()[bcRegion]->
                              UpdatePhys())[id1], 1);
             }
         }
     }

void Nektar::EulerCFE::SetBoundaryRinglebFlow	(	int	bcRegion,
		NekDouble	time,
		int	cnt,
		Array< OneD, Array< OneD, NekDouble > > &	physarray
	)

private

Set the boundary conditions for the Ringleb flow problem.

Definition at line 833 of file EulerCFE.cpp.

References Nektar::LibUtilities::eFunctionTypeFile, Nektar::SolverUtils::EquationSystem::eHomogeneous1D, Nektar::SolverUtils::EquationSystem::GetTraceTotPoints(), Nektar::SolverUtils::EquationSystem::m_expdim, Nektar::SolverUtils::EquationSystem::m_fields, Nektar::CompressibleFlowSystem::m_gamma, Nektar::SolverUtils::EquationSystem::m_HomogeneousType, Nektar::SolverUtils::EquationSystem::m_session, and Vmath::Vcopy().

Referenced by SetBoundaryConditions().

     {
         int nvariables      = physarray.num_elements();
         int nTraceNumPoints = GetTraceTotPoints();
         Array<OneD, Array<OneD, NekDouble> > Fwd(nvariables);
         
         // For 3DHomogenoeus1D
         int n_planes = 1;
         if (m_expdim == 2 &&  m_HomogeneousType == eHomogeneous1D)
         {
             int nPointsTot = m_fields[0]->GetTotPoints();
             int nPointsTot_plane = m_fields[0]->GetPlane(0)->GetTotPoints();
             n_planes = nPointsTot/nPointsTot_plane;
             nTraceNumPoints = nTraceNumPoints * n_planes;
         }
         
         // Get physical values of the forward trace (from exp to phys)
         for (int i = 0; i < nvariables; ++i)
         {
             Fwd[i] = Array<OneD, NekDouble>(nTraceNumPoints);
             m_fields[i]->ExtractTracePhys(physarray[i], Fwd[i]);
         }
         
         int id2, id2_plane, e_max;
         
         e_max = m_fields[0]->GetBndCondExpansions()[bcRegion]->GetExpSize();
         
         for(int e = 0; e < e_max; ++e)
         {
             int npoints = m_fields[0]->
             GetBndCondExpansions()[bcRegion]->GetExp(e)->GetTotPoints();
             int id1  = m_fields[0]->
             GetBndCondExpansions()[bcRegion]->GetPhys_Offset(e);
             
             // For 3DHomogenoeus1D
             if (m_expdim == 2 &&  m_HomogeneousType == eHomogeneous1D)
             {
                 int cnt_plane = cnt/n_planes;
                 int e_plane;
                 int e_max_plane = e_max/n_planes;
                 int nTracePts_plane = GetTraceTotPoints();
                 
                 int planeID = floor((e + 0.5 )/ e_max_plane );
                 e_plane = e - e_max_plane*planeID;
                 
                 id2_plane  = m_fields[0]->GetTrace()->GetPhys_Offset(
                     m_fields[0]->GetTraceMap()->
                     GetBndCondCoeffsToGlobalCoeffsMap(
                         cnt_plane + e_plane));
                 id2 = id2_plane + planeID*nTracePts_plane;
             }
             else // For general case
             {
                 id2 = m_fields[0]->
                 GetTrace()->GetPhys_Offset(m_fields[0]->GetTraceMap()->
                 GetBndCondTraceToGlobalTraceMap(cnt++));
             }
             
             Array<OneD,NekDouble> x0(npoints, 0.0);
             Array<OneD,NekDouble> x1(npoints, 0.0);
             Array<OneD,NekDouble> x2(npoints, 0.0);
             
             m_fields[0]->GetBndCondExpansions()[bcRegion]->
             GetExp(e)->GetCoords(x0, x1, x2);
             
             // Flow parameters
             NekDouble c, k, phi, r, J, VV, pp, sint, P, ss;
             NekDouble J11, J12, J21, J22, det;
             NekDouble Fx, Fy;
             NekDouble xi, yi;
             NekDouble dV;
             NekDouble dtheta;
             NekDouble par1;
             NekDouble theta     = M_PI / 4.0;
             NekDouble kExt      = 0.7;
             NekDouble V         = kExt * sin(theta);
             NekDouble toll      = 1.0e-8;
             NekDouble errV      = 1.0;
             NekDouble errTheta  = 1.0;
             NekDouble gamma     = m_gamma;
             NekDouble gamma_1_2 = (gamma - 1.0) / 2.0;
             
             // Loop on all the points of that edge
             for (int j = 0; j < npoints; j++)
             {
                 
                 while ((abs(errV) > toll) || (abs(errTheta) > toll))
                 {
                     VV   = V * V;
                     sint = sin(theta);
                     c    = sqrt(1.0 - gamma_1_2 * VV);
                     k    = V / sint;
                     phi  = 1.0 / k;
                     pp   = phi * phi;
                     J    = 1.0 / c + 1.0 / (3.0 * c * c * c) + 
                     1.0 / (5.0 * c * c * c * c * c) - 
                     0.5 * log((1.0 + c) / (1.0 - c));
                     
                     r    = pow(c, 1.0 / gamma_1_2);
                     xi   = 1.0 / (2.0 * r) * (1.0 / VV - 2.0 * pp) + J / 2.0;
                     yi   = phi / (r * V) * sqrt(1.0 - VV * pp);
                     par1 = 25.0 - 5.0 * VV;
                     ss   = sint * sint;
                     
                     Fx   = xi - x0[j];
                     Fy   = yi - x1[j];
                     
                     J11 = 39062.5 / pow(par1, 3.5) * 
                     (1.0 / VV - 2.0 / VV * ss) * V + 1562.5 / 
                     pow(par1, 2.5) * (-2.0 / (VV * V) + 4.0 / 
                     (VV * V) * ss) + 12.5 / pow(par1, 1.5) * V + 
                     312.5 / pow(par1, 2.5) * V + 7812.5 / 
                     pow(par1, 3.5) * V - 0.25 * 
                     (-1.0 / pow(par1, 0.5) * V / (1.0 - 0.2 * 
                     pow(par1, 0.5)) - (1.0 + 0.2 * pow(par1, 0.5)) / 
                     pow((1.0 - 0.2 * pow(par1, 0.5)), 2.0) / 
                     pow(par1, 0.5) * V) / (1.0 + 0.2 * pow(par1, 0.5)) *
                     (1.0 - 0.2 * pow(par1, 0.5));
                     
                     J12 = -6250.0 / pow(par1, 2.5) / VV * sint * cos(theta);
                     J21 = -6250.0 / (VV * V) * sint / pow(par1, 2.5) * 
                     pow((1.0 - ss), 0.5) + 78125.0 / V * sint / 
                     pow(par1, 3.5) * pow((1.0 - ss), 0.5);
                     
                     // the matrix is singular when theta = pi/2
                     if (abs(x1[j]) < toll && abs(cos(theta)) < toll)
                     {
                         J22 = -39062.5 / pow(par1, 3.5) / V + 3125 / 
                         pow(par1, 2.5) / (VV * V) + 12.5 / 
                         pow(par1, 1.5) * V + 312.5 / pow(par1, 2.5) * 
                         V + 7812.5 / pow(par1, 3.5) * V - 0.25 * 
                         (-1.0 / pow(par1, 0.5) * V / (1.0 - 0.2 * 
                         pow(par1, 0.5)) - (1.0 + 0.2 * pow(par1, 0.5)) /
                         pow((1.0 - 0.2 * pow(par1, 0.5)), 2.0) / 
                         pow(par1, 0.5) * V) / (1.0 + 0.2 * 
                         pow(par1, 0.5)) * (1.0 - 0.2 * pow(par1, 0.5));
                         
                         // dV = -dV/dx * Fx
                         dV      = -1.0 / J22 * Fx;
                         dtheta  = 0.0;
                         theta   = M_PI / 2.0;
                     }
                     else
                     {
                         J22 = 3125.0 / VV * cos(theta) / pow(par1, 2.5) * 
                         pow((1.0 - ss), 0.5) - 3125.0 / VV * ss / 
                         pow(par1, 2.5) / pow((1.0 - ss), 0.5) * 
                         cos(theta);
                         
                         det = -1.0 / (J11 * J22 - J12 * J21);
                         
                         // [dV dtheta]' = -[invJ]*[Fx Fy]'
                         dV     = det * ( J22 * Fx - J12 * Fy);
                         dtheta = det * (-J21 * Fx + J11 * Fy);
                     }
                     
                     V     = V + dV;
                     theta = theta + dtheta;
                     
                     errV     = abs(dV);
                     errTheta = abs(dtheta);
                 }
                 
                 c                      = sqrt(1.0 - gamma_1_2 * VV);
                 int kk                 = id2 + j;
                 NekDouble timeramp     = 200.0;
                 std::string restartstr = "RESTART";
                 if (time<timeramp &&
                     !(m_session->DefinesFunction("InitialConditions") &&
                     m_session->GetFunctionType("InitialConditions", 0) ==
                     LibUtilities::eFunctionTypeFile))
                 {
                     Fwd[0][kk] = pow(c, 1.0 / gamma_1_2) * 
                     exp(-1.0 + time /timeramp);
                     
                     Fwd[1][kk] = Fwd[0][kk] * V * cos(theta) * 
                     exp(-1 + time / timeramp);
                     
                     Fwd[2][kk] = Fwd[0][kk] * V * sin(theta) * 
                     exp(-1 + time / timeramp);
                 }
                 else
                 {
                     Fwd[0][kk]  = pow(c, 1.0 / gamma_1_2);
                     Fwd[1][kk] = Fwd[0][kk] * V * cos(theta);
                     Fwd[2][kk] = Fwd[0][kk] * V * sin(theta);
                 }
                 
                 P  = (c * c) * Fwd[0][kk] / gamma;
                 Fwd[3][kk]  = P / (gamma - 1.0) + 0.5 * 
                 (Fwd[1][kk] * Fwd[1][kk] / Fwd[0][kk] + 
                 Fwd[2][kk] * Fwd[2][kk] / Fwd[0][kk]);
                 
                 errV     = 1.0;
                 errTheta = 1.0;
                 theta    = M_PI / 4.0;
                 V        = kExt * sin(theta);
             }
             
             for (int i = 0; i < nvariables; ++i)
             {
                 Vmath::Vcopy(npoints, &Fwd[i][id2], 1, 
                              &(m_fields[i]->GetBndCondExpansions()[bcRegion]->
                              UpdatePhys())[id1],1);
             }
         }
     }

void Nektar::EulerCFE::SetInitialIsentropicVortex ( NekDouble initialtime )

private

Set the initial condition for the isentropic vortex problem.

Definition at line 358 of file EulerCFE.cpp.

References EvaluateIsentropicVortex(), Nektar::SolverUtils::EquationSystem::GetTotPoints(), Nektar::SolverUtils::EquationSystem::m_fields, Nektar::SolverUtils::EquationSystem::m_spacedim, and Vmath::Vcopy().

Referenced by v_SetInitialConditions().

     {
         int nTotQuadPoints  = GetTotPoints();
         Array<OneD, NekDouble> x(nTotQuadPoints);
         Array<OneD, NekDouble> y(nTotQuadPoints);
         Array<OneD, NekDouble> z(nTotQuadPoints);
         Array<OneD, Array<OneD, NekDouble> > u(m_spacedim+2);
         
         m_fields[0]->GetCoords(x, y, z);
         
         for (int i = 0; i < m_spacedim + 2; ++i)
         {
             u[i] = Array<OneD, NekDouble>(nTotQuadPoints);
         }
         
         EvaluateIsentropicVortex(x, y, z, u, initialtime);
         
         // Forward transform to fill the coefficient space
         for(int i = 0; i < m_fields.num_elements(); ++i)
         {
             Vmath::Vcopy(nTotQuadPoints, u[i], 1, m_fields[i]->UpdatePhys(), 1);
             m_fields[i]->SetPhysState(true);
             m_fields[i]->FwdTrans(m_fields[i]->GetPhys(), 
                                   m_fields[i]->UpdateCoeffs());
         }
     }

void Nektar::EulerCFE::SetInitialRinglebFlow ( void )

private

Set the initial condition for the Ringleb flow problem.

Definition at line 589 of file EulerCFE.cpp.

References Nektar::SolverUtils::EquationSystem::m_fields, Nektar::CompressibleFlowSystem::m_gamma, Nektar::SolverUtils::EquationSystem::m_sessionName, and Nektar::SolverUtils::EquationSystem::WriteFld().

     {
         // Get number of different boundaries in the input file
         int nbnd    = m_fields[0]->GetBndConditions().num_elements();
         
         // Loop on all the edges of the input file
         for(int bcRegion=0; bcRegion < nbnd; ++bcRegion)
         {
             
             int npoints = m_fields[0]->
             GetBndCondExpansions()[bcRegion]->GetNpoints();
             
             Array<OneD,NekDouble> x0(npoints, 0.0);
             Array<OneD,NekDouble> x1(npoints, 0.0);
             Array<OneD,NekDouble> x2(npoints, 0.0);
             
             Array<OneD, NekDouble> rho(npoints,  0.0);
             Array<OneD, NekDouble> rhou(npoints, 0.0);
             Array<OneD, NekDouble> rhov(npoints, 0.0);
             Array<OneD, NekDouble> E(npoints,    0.0);
             
             m_fields[0]->GetBndCondExpansions()[bcRegion]->
             GetCoords(x0, x1, x2);
             
             // Flow parameters
             NekDouble c, k, phi, r, J, VV, pp, sint, P, ss;
             NekDouble J11, J12, J21, J22, det;
             NekDouble Fx, Fy;
             NekDouble xi, yi;
             NekDouble dV;
             NekDouble dtheta;
             NekDouble par1;
             NekDouble theta     = M_PI / 4.0;
             NekDouble kExt      = 0.7;
             NekDouble V         = kExt * sin(theta);
             NekDouble toll      = 1.0e-8;
             NekDouble errV      = 1.0;
             NekDouble errTheta  = 1.0;
             NekDouble gamma     = m_gamma;
             NekDouble gamma_1_2 = (gamma - 1.0) / 2.0;
             
             // Loop on all the points of that edge
             for (int j = 0; j < npoints; j++)
             {
                 while ((abs(errV) > toll) || (abs(errTheta) > toll))
                 {
                     
                     VV   = V * V;
                     sint = sin(theta);
                     c    = sqrt(1.0 - gamma_1_2 * VV);
                     k    = V / sint;
                     phi  = 1.0 / k;
                     pp   = phi * phi;
                     J    = 1.0 / c + 1.0 / (3.0 * c * c * c) + 
                     1.0 / (5.0 * c * c * c * c * c) - 
                     0.5 * log((1.0 + c) / (1.0 - c));
                     
                     r    = pow(c, 1.0 / gamma_1_2);
                     xi   = 1.0 / (2.0 * r) * (1.0 / VV - 2.0 * pp) + J / 2.0;
                     yi   = phi / (r * V) * sqrt(1.0 - VV * pp);
                     par1 = 25.0 - 5.0 * VV;
                     ss   = sint * sint;
                     
                     Fx = xi - x0[j];
                     Fy = yi - x1[j];
                     
                     J11 = 39062.5 / pow(par1, 3.5) * 
                     (1.0 / VV - 2.0 / VV * ss) * V + 
                     1562.5 / pow(par1, 2.5) * (-2.0 / 
                     (VV * V) + 4.0 / (VV * V) * ss) + 
                     12.5 / pow(par1, 1.5) * V + 
                     312.5 / pow(par1, 2.5) * V + 
                     7812.5 / pow(par1, 3.5) * V - 
                     0.25 * (-1.0 / pow(par1, 0.5) * V / 
                     (1.0 - 0.2 * pow(par1, 0.5)) - (1.0 + 0.2 * 
                     pow(par1, 0.5)) / pow((1.0 - 0.2 * 
                     pow(par1, 0.5)), 2.0) / 
                     pow(par1, 0.5) * V) / 
                     (1.0 + 0.2 * pow(par1, 0.5)) * 
                     (1.0 - 0.2 * pow(par1, 0.5));
                     
                     J12 = -6250.0 / pow(par1, 2.5) / VV * sint * cos(theta);
                     J21 = -6250.0 / (VV * V) * sint / pow(par1, 2.5) * 
                     pow((1.0 - ss), 0.5) + 78125.0 / V * sint / 
                     pow(par1, 3.5) * pow((1.0 - ss), 0.5);
                     
                     // the matrix is singular when theta = pi/2
                     if (abs(x1[j]) < toll && abs(cos(theta)) < toll)
                     {
                         
                         J22 = -39062.5 / pow(par1, 3.5) / V +
                         3125 / pow(par1, 2.5) / (VV * V) + 12.5 / 
                         pow(par1, 1.5) * V + 312.5 / pow(par1, 2.5) * V + 
                         7812.5 / pow(par1, 3.5) * V - 
                         0.25 * (-1.0 / pow(par1, 0.5) * V / 
                         (1.0 - 0.2 * pow(par1, 0.5)) - 
                         (1.0 + 0.2 * pow(par1, 0.5)) / 
                         pow((1.0 - 0.2*  pow(par1, 0.5)), 2.0) / 
                         pow(par1, 0.5) *V) / 
                         (1.0 + 0.2 * pow(par1, 0.5)) * 
                         (1.0 - 0.2 * pow(par1, 0.5));
                         
                         // dV = -dV/dx * Fx
                         dV     = -1.0 / J22 * Fx;
                         dtheta = 0.0;
                         theta  = M_PI / 2.0;
                     }
                     else
                     {
                         
                         J22 = 3125.0 / VV * cos(theta) / pow(par1, 2.5) * 
                         pow((1.0 - ss), 0.5) - 3125.0 / VV * ss / 
                         pow(par1, 2.5) / pow((1.0 - ss), 0.5) * 
                         cos(theta);
                         
                         det = -1.0 / (J11 * J22 - J12 * J21);
                         
                         // [dV dtheta]' = -[invJ]*[Fx Fy]'
                         dV     = det * ( J22 * Fx - J12 * Fy);
                         dtheta = det * (-J21 * Fx + J11 * Fy);
                     }
                     
                     V     = V + dV;
                     theta = theta + dtheta;
                     
                     errV     = abs(dV);
                     errTheta = abs(dtheta);
                     
                 }
                 
                 c        = sqrt(1.0 - gamma_1_2 * VV);
                 rho[j]   = pow(c, 1.0 / gamma_1_2) * exp(-1.0);
                 rhou[j]  = rho[j] * V * cos(theta) * exp(-1.0);
                 rhov[j]  = rho[j] * V * sin(theta) * exp(-1.0);
                 P        = (c * c) * rho[j] / gamma;
                 E[j]     = P / (gamma - 1.0) + 0.5 * 
                 (rhou[j] * rhou[j] / 
                 rho[j] + rhov[j] * rhov[j] / rho[j]);
                 errV     = 1.0;
                 errTheta = 1.0;
                 theta    = M_PI / 4.0;
                 V        = kExt * sin(theta);
                 
             }
             
             // Fill the physical space
             m_fields[0]->GetBndCondExpansions()[bcRegion]->SetPhys(rho);
             m_fields[1]->GetBndCondExpansions()[bcRegion]->SetPhys(rhou);
             m_fields[2]->GetBndCondExpansions()[bcRegion]->SetPhys(rhov);
             m_fields[3]->GetBndCondExpansions()[bcRegion]->SetPhys(E);
             
             // Forward transform to fill the coefficients space
             for(int i = 0; i < m_fields.num_elements(); ++i)
             {
                 m_fields[i]->GetBndCondExpansions()[bcRegion]->
                 FwdTrans_BndConstrained(
                     m_fields[i]->GetBndCondExpansions()[bcRegion]->
                     GetPhys(),
                                         m_fields[i]->GetBndCondExpansions()[bcRegion]->
                                         UpdateCoeffs());
             }
             
         }
         
         // Calculation of the initial internal values as a weighted average 
         // over the distance from the boundaries
         int nq = m_fields[0]->GetNpoints();
         
         Array<OneD,NekDouble> x0(nq);
         Array<OneD,NekDouble> x1(nq);
         Array<OneD,NekDouble> x2(nq);
         
         // Get the coordinates 
         // (assuming all fields have the same discretisation)
         m_fields[0]->GetCoords(x0, x1, x2);
         
         for(int j = 0; j < nq; j++)
         {
             NekDouble Dist    = 0.0;
             NekDouble rho     = 0.0;
             NekDouble rhou    = 0.0;
             NekDouble rhov    = 0.0;
             NekDouble E       = 0.0;
             NekDouble SumDist = 0.0;
             
             // Calculation of all the distances
             // Loop on all the edges of the input file
             for (int bcRegion = 0; bcRegion < nbnd; ++bcRegion)
             {
                 // Get quadrature points on the edge
                 int npoints = m_fields[0]->
                 GetBndCondExpansions()[bcRegion]->GetNpoints();
                 
                 Array<OneD,NekDouble> xb0(npoints, 0.0);
                 Array<OneD,NekDouble> xb1(npoints, 0.0);
                 Array<OneD,NekDouble> xb2(npoints, 0.0);
                 
                 m_fields[0]->GetBndCondExpansions()[bcRegion]->
                 GetCoords(xb0, xb1, xb2);
                 
                 for (int k = 0; k < npoints; k++)
                 {
                     Dist = sqrt((xb0[k] - x0[j]) * (xb0[k] - x0[j]) + 
                     (xb1[k] - x1[j]) * (xb1[k] - x1[j]));
                     
                     SumDist += Dist;
                     rho     += Dist * (m_fields[0]->
                     GetBndCondExpansions()[bcRegion]->GetPhys())[k];
                     rhou    += Dist * (m_fields[1]->
                     GetBndCondExpansions()[bcRegion]->GetPhys())[k];
                     rhov    += Dist * (m_fields[2]->
                     GetBndCondExpansions()[bcRegion]->GetPhys())[k];
                     E       += Dist * (m_fields[3]->
                     GetBndCondExpansions()[bcRegion]->GetPhys())[k];
                 }
             }
             
             rho  = rho / SumDist;
             rhou = rhou / SumDist;
             rhov = rhov / SumDist;
             E    = E / SumDist;
             
             (m_fields[0]->UpdatePhys())[j] = rho;
             (m_fields[1]->UpdatePhys())[j] = rhou;
             (m_fields[2]->UpdatePhys())[j] = rhov;
             (m_fields[3]->UpdatePhys())[j] = E;
             
         }
         
         for (int i = 0 ; i < m_fields.num_elements(); i++)
         {
             m_fields[i]->SetPhysState(true);
             m_fields[i]->FwdTrans(m_fields[i]->GetPhys(), 
                                   m_fields[i]->UpdateCoeffs());
         }
         
         // Dump initial conditions to file
         std::string outname = m_sessionName + "_initialRingleb.chk";
         WriteFld(outname);
     }

void Nektar::EulerCFE::v_EvaluateExactSolution	(	unsigned int	field,
		Array< OneD, NekDouble > &	outfield,
		const NekDouble	time = `0.0`
	)

protectedvirtual

Get the exact solutions for isentropic vortex and Ringleb flow problems.

Reimplemented from Nektar::SolverUtils::EquationSystem.

Definition at line 263 of file EulerCFE.cpp.

References Nektar::eIsentropicVortex, Nektar::eRinglebFlow, GetExactIsentropicVortex(), GetExactRinglebFlow(), and m_problemType.

     {
         switch(m_problemType)
         {
             case eIsentropicVortex:
             {
                 GetExactIsentropicVortex(field, outfield, time);
                 break;
             }
             case eRinglebFlow:
             {
                 GetExactRinglebFlow(field, outfield);
                 break;
             }
             default:
             {
                 EquationSystem::v_EvaluateExactSolution(field, outfield, time);
                 break;
             }
         }
     }

void Nektar::EulerCFE::v_GenerateSummary ( SolverUtils::SummaryList & s )

protectedvirtual

Print a summary of time stepping parameters.

Print out a summary with some relevant information.

Reimplemented from Nektar::CompressibleFlowSystem.

Definition at line 102 of file EulerCFE.cpp.

References Nektar::SolverUtils::AddSummaryItem(), m_problemType, Nektar::ProblemTypeMap, and Nektar::CompressibleFlowSystem::v_GenerateSummary().

     {
         CompressibleFlowSystem::v_GenerateSummary(s);
         SolverUtils::AddSummaryItem(s, "Problem Type", ProblemTypeMap[m_problemType]);
     }

void Nektar::EulerCFE::v_InitObject ( )

protectedvirtual

Initialization object for CompressibleFlowSystem class.

Reimplemented from Nektar::CompressibleFlowSystem.

Definition at line 58 of file EulerCFE.cpp.

References ASSERTL0, Nektar::LibUtilities::TimeIntegrationSchemeOperators::DefineOdeRhs(), Nektar::LibUtilities::TimeIntegrationSchemeOperators::DefineProjection(), DoOdeProjection(), DoOdeRhs(), Nektar::SolverUtils::UnsteadySystem::m_explicitAdvection, Nektar::SolverUtils::UnsteadySystem::m_ode, m_problemType, Nektar::SolverUtils::EquationSystem::m_session, Nektar::ProblemTypeMap, Nektar::SIZE_ProblemType, and Nektar::CompressibleFlowSystem::v_InitObject().

     {
         CompressibleFlowSystem::v_InitObject();
         
         if(m_session->DefinesSolverInfo("PROBLEMTYPE"))
         {
             int i;
             std::string ProblemTypeStr = 
             m_session->GetSolverInfo("PROBLEMTYPE");
             for (i = 0; i < (int) SIZE_ProblemType; ++i)
             {
                 if (boost::iequals(ProblemTypeMap[i], ProblemTypeStr))
                 {
                     m_problemType = (ProblemType)i;
                     break;
                 }
             }
         }
         else
         {
             m_problemType = (ProblemType)0;
         }
         
         if (m_explicitAdvection)
         {
             m_ode.DefineOdeRhs     (&EulerCFE::DoOdeRhs,        this);
             m_ode.DefineProjection (&EulerCFE::DoOdeProjection, this);
         }
         else
         {
             ASSERTL0(false, "Implicit CFE not set up.");
         }
     }

void Nektar::EulerCFE::v_SetInitialConditions	(	NekDouble	initialtime = `0.0`,
		bool	dumpInitialConditions = `true`,
		const int	domain = `0`
	)

protectedvirtual

Set the initial conditions.

Reimplemented from Nektar::CompressibleFlowSystem.

Definition at line 111 of file EulerCFE.cpp.

References Nektar::SolverUtils::EquationSystem::Checkpoint_Output(), Nektar::eIsentropicVortex, Nektar::SolverUtils::EquationSystem::m_checksteps, m_problemType, SetInitialIsentropicVortex(), and Nektar::CompressibleFlowSystem::v_SetInitialConditions().

     {
         switch (m_problemType)
         {
             case eIsentropicVortex:
             {
                 SetInitialIsentropicVortex(initialtime);
                 break;
             }
             default:
             {
                 EquationSystem::v_SetInitialConditions(initialtime, false);
                 break;
             }
         }
 
         CompressibleFlowSystem::v_SetInitialConditions();
 
         if (dumpInitialConditions && m_checksteps)
         {
             // Dump initial conditions to file
             Checkpoint_Output(0);
         }
     }

Friends And Related Function Documentation

friend class MemoryManager< EulerCFE >

friend

Definition at line 61 of file EulerCFE.h.

Member Data Documentation

string Nektar::EulerCFE::className

static

Initial value:

= 
    SolverUtils::GetEquationSystemFactory().RegisterCreatorFunction(
        "EulerCFE", EulerCFE::create, 
        "Euler equations in conservative variables without "
        "artificial diffusion.")

Name of class.

Definition at line 72 of file EulerCFE.h.

ProblemType Nektar::EulerCFE::m_problemType

Definition at line 77 of file EulerCFE.h.

Referenced by v_EvaluateExactSolution(), v_GenerateSummary(), v_InitObject(), and v_SetInitialConditions().

Public Member Functions

Static Public Member Functions

Public Attributes

Static Public Attributes

Protected Member Functions

Private Member Functions

Friends

Additional Inherited Members

Detailed Description

Constructor & Destructor Documentation

Member Function Documentation

Friends And Related Function Documentation

Member Data Documentation