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ReducedCompressibleSteadyNS Class Reference

Class where it is implemented a reduced problem for the steady Navier-stokes problem. More...

#include <ReducedCompressibleSteadyNS.H>

Inheritance diagram for ReducedCompressibleSteadyNS:
ReducedSteadyNSTurb reducedSteadyNS reducedProblem ReducedCompressibleSteadyNN ReducedCompressibleSteadyNN

Public Member Functions

 ReducedCompressibleSteadyNS ()
 Construct Null.
 
 ReducedCompressibleSteadyNS (CompressibleSteadyNS &problem)
 Construct Null.
 
 ~ReducedCompressibleSteadyNS ()
 
void solveOnlineCompressible (scalar mu_now, int NmodesUproj, int NmodesPproj, int NmodesEproj)
 Method to perform an online solve using a PPE stabilisation method.
 
void setOnlineVelocity (Eigen::MatrixXd vel)
 It checks if the number of imposed boundary conditions is correct and set the inlet velocity equal to the given one.
 
void projectReducedOperators (int NmodesUproj, int NmodesPproj, int NmodesEproj)
 It assembles the reduced oeprators using the modes.
 
- Public Member Functions inherited from ReducedSteadyNSTurb
 ReducedSteadyNSTurb ()
 Construct Null.
 
 ReducedSteadyNSTurb (SteadyNSTurb &problem)
 Construct Null.
 
 ~ReducedSteadyNSTurb ()
 
void solveOnlineSUP (Eigen::MatrixXd velNow)
 Method to perform an online solve using a supremizer stabilisation method.
 
void solveOnlinePPE (Eigen::MatrixXd velNow)
 Method to perform an online solve using a PPE stabilisation method.
 
void reconstruct (bool exportFields=false, fileName folder="./ITHACAoutput/online_rec", int printevery=1)
 Method to reconstruct the solutions from an online solve.
 
Eigen::MatrixXd setOnlineVelocity (Eigen::MatrixXd vel)
 Sets the online velocity.
 
- Public Member Functions inherited from reducedSteadyNS
 reducedSteadyNS ()
 Construct Null.
 
 reducedSteadyNS (steadyNS &problem)
 Construct Null.
 
 ~reducedSteadyNS ()
 
void solveOnline_PPE (Eigen::MatrixXd vel_now)
 Method to perform an online solve using a PPE stabilisation method.
 
void solveOnline_sup (Eigen::MatrixXd vel_now)
 Method to perform an online solve using a supremizer stabilisation method.
 
void reconstruct_PPE (fileName folder="./ITHACAoutput/online_rec", int printevery=1)
 Method to reconstruct a solution from an online solve with a PPE stabilisation technique.
 
void reconstruct (bool exportFields=false, fileName folder="./ITHACAoutput/online_rec", int printevery=1)
 Method to reconstruct the solutions from an online solve.
 
void reconstructLiftAndDrag (steadyNS &problem, fileName folder)
 Method to compute the reduced order forces.
 
double inf_sup_constant ()
 Method to evaluate the online inf-sup constant.
 
Eigen::MatrixXd setOnlineVelocity (Eigen::MatrixXd vel)
 Sets the online velocity.
 
- Public Member Functions inherited from reducedProblem
 reducedProblem ()
 Construct Null.
 
virtual ~reducedProblem ()
 
 reducedProblem (reductionProblem &problem)
 Construct with reduced Problem.
 
virtual void solveOnline ()
 Virtual Method to perform and online Solve.
 

Public Attributes

volVectorModes ULmodes
 Lifted velocity modes.
 
CompressibleSteadyNSproblem
 Full problem.
 
Eigen::MatrixXd vel_now
 Imposed boundary conditions.
 
int counter = 0
 Counter.
 
Eigen::MatrixXd projGradModP
 Projected gradient of the pressure modes.
 
- Public Attributes inherited from ReducedSteadyNSTurb
PtrList< volScalarField > nutFields
 List of snapshots for the solution for eddy viscosity.
 
PtrList< volScalarField > nutModes
 List of POD modes for eddy viscosity.
 
Eigen::MatrixXd rbfCoeffMat
 The matrix of the eddy viscosity RBF interoplated coefficients.
 
Eigen::VectorXd rbfCoeff
 Vector of eddy viscosity RBF interoplated coefficients.
 
int nphiNut
 Number of viscosity modes.
 
newtonSteadyNSTurbSUP newtonObjectSUP
 Newton Object to solve the nonlinear problem sup approach.
 
newtonSteadyNSTurbPPE newtonObjectPPE
 Newton Object to solve the nonlinear problem PPE approach.
 
SteadyNSTurbproblem
 Pointer to the FOM problem.
 
PtrList< volScalarField > nutRecFields
 Reconstructed eddy viscosity fields list.
 
- Public Attributes inherited from reducedSteadyNS
ITHACAparameterspara
 parameters to be read from the ITHACAdict file
 
Eigen::MatrixXd vel_now
 Online inlet velocity vector.
 
Eigen::MatrixXd fTau
 Reduced matrix for tangent forces.
 
Eigen::MatrixXd fN
 Reduced matrix for normal forces.
 
Eigen::VectorXd y_old
 Vector to store the previous solution during the Newton procedure.
 
Eigen::VectorXd y
 Vector to store the solution during the Newton procedure.
 
scalar nu
 Reduced viscosity in case of parametrized viscosity.
 
List< Eigen::MatrixXd > online_solution
 List of Eigen matrices to store the online solution.
 
PtrList< volVectorField > Umodes
 List of pointers to store the modes for velocity.
 
PtrList< volScalarField > Pmodes
 List of pointers to store the modes for pressure.
 
PtrList< volVectorField > Usnapshots
 List of pointers to store the snapshots for velocity.
 
PtrList< volScalarField > Psnapshots
 List of pointers to store the snapshots for pressure.
 
PtrList< volScalarField > PREC
 Reconstructed pressure field.
 
PtrList< volVectorField > UREC
 Recontructed velocity field.
 
PtrList< volScalarField > pRecFields
 Reconstructed pressure fields list.
 
PtrList< volVectorField > uRecFields
 Recontructed velocity fields list.
 
newton_steadyNS newton_object
 Newton object used to solve the non linear problem.
 
steadyNSproblem
 Pointer to the FOM problem.
 
int Nphi_u
 Number of velocity modes.
 
int Nphi_p
 Number of pressure modes.
 
int Nphi_sup
 Number of supremizer modes.
 
int N_BC
 Number of parametrized boundary conditions.
 
int count_online_solve = 1
 Counter to count the online solutions.
 
Eigen::MatrixXd tauU
 Penalty Factor.
 
- Public Attributes inherited from reducedProblem
scalar nu
 Viscosity.
 
reductionProblemproblem
 Pointer to FOAM problem.
 

Additional Inherited Members

- Static Public Member Functions inherited from reducedProblem
static Eigen::MatrixXd solveLinearSys (List< Eigen::MatrixXd > LinSys, Eigen::MatrixXd x, Eigen::VectorXd &residual, const Eigen::MatrixXd &bc=Eigen::MatrixXd::Zero(0, 0), const std::string solverType="fullPivLu")
 Linear system solver for the online problem.
 
static Eigen::MatrixXd solveLinearSys (List< Eigen::MatrixXd > LinSys, Eigen::MatrixXd x, Eigen::VectorXd &residual, const std::string solverType)
 Linear system solver for the online problem.
 

Detailed Description

Class where it is implemented a reduced problem for the steady Navier-stokes problem.

In this class are implemented the methods to solve a reduced version of the stationary Navier-stokes equations. This class must be used together with the steadyNS class

Definition at line 62 of file ReducedCompressibleSteadyNS.H.

Constructor & Destructor Documentation

◆ ReducedCompressibleSteadyNS() [1/2]

ReducedCompressibleSteadyNS::ReducedCompressibleSteadyNS ( )

Construct Null.

Definition at line 39 of file ReducedCompressibleSteadyNS.C.

◆ ReducedCompressibleSteadyNS() [2/2]

ReducedCompressibleSteadyNS::ReducedCompressibleSteadyNS ( CompressibleSteadyNS & problem)
explicit

Construct Null.

Parameters
[in]problema full order steadyNS problem
[in]tipoType of pressure stabilisation method you want to use "SUP" for supremizer, "PPE" for pressure Poisson equation.

Definition at line 43 of file ReducedCompressibleSteadyNS.C.

◆ ~ReducedCompressibleSteadyNS()

ReducedCompressibleSteadyNS::~ReducedCompressibleSteadyNS ( )
inline

Definition at line 78 of file ReducedCompressibleSteadyNS.H.

Member Function Documentation

◆ projectReducedOperators()

void ReducedCompressibleSteadyNS::projectReducedOperators ( int NmodesUproj,
int NmodesPproj,
int NmodesEproj )

It assembles the reduced oeprators using the modes.

Parameters
[in]NmodesUprojThe number of modes one wants to use for velocity projection.
[in]NmodesPprojThe number of modes one wants to use for pressure projection.
[in]NmodesEprojThe number of modes one wants to use for energy projection.

Definition at line 81 of file ReducedCompressibleSteadyNS.C.

◆ setOnlineVelocity()

void ReducedCompressibleSteadyNS::setOnlineVelocity ( Eigen::MatrixXd vel)

It checks if the number of imposed boundary conditions is correct and set the inlet velocity equal to the given one.

Parameters
[in]velInlet velocity

Definition at line 60 of file ReducedCompressibleSteadyNS.C.

◆ solveOnlineCompressible()

void ReducedCompressibleSteadyNS::solveOnlineCompressible ( scalar mu_now,
int NmodesUproj,
int NmodesPproj,
int NmodesEproj )

Method to perform an online solve using a PPE stabilisation method.

Parameters
[in]mu_nowThe online viscosity.
[in]NmodesUprojThe number of modes one wants to use for velocity projection.
[in]NmodesPprojThe number of modes one wants to use for pressure projection.
[in]NmodesEprojThe number of modes one wants to use for energy projection.

Definition at line 96 of file ReducedCompressibleSteadyNS.C.

Member Data Documentation

◆ counter

int ReducedCompressibleSteadyNS::counter = 0

Counter.

Definition at line 127 of file ReducedCompressibleSteadyNS.H.

◆ problem

CompressibleSteadyNS* ReducedCompressibleSteadyNS::problem

Full problem.

Definition at line 121 of file ReducedCompressibleSteadyNS.H.

◆ projGradModP

Eigen::MatrixXd ReducedCompressibleSteadyNS::projGradModP

Projected gradient of the pressure modes.

Definition at line 132 of file ReducedCompressibleSteadyNS.H.

◆ ULmodes

volVectorModes ReducedCompressibleSteadyNS::ULmodes

Lifted velocity modes.

Definition at line 112 of file ReducedCompressibleSteadyNS.H.

◆ vel_now

Eigen::MatrixXd ReducedCompressibleSteadyNS::vel_now

Imposed boundary conditions.

Definition at line 124 of file ReducedCompressibleSteadyNS.H.


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