1 //============================================================================
4 * \author Michael NDJINGA, Kieu Nguyen
7 * \brief The compressible Navier-Stokes equations
9 //============================================================================
11 /*! \class SinglePhase SinglePhase.hxx "SinglePhase.hxx"
12 * \brief The compressible Navier-Stokes equations
13 * \details The model consists in one mass, one momentum and one energy equation, see \ref NSModelsPage for more details
15 #ifndef SINGLEPHASE_HXX_
16 #define SINGLEPHASE_HXX_
18 #include "ProblemFluid.hxx"
20 class SinglePhase : public ProblemFluid{
23 * \brief Constructor for the Navier-Stokes system
24 * \param [in] phaseType : \ref Liquid or \ref Gas
25 * \param [in] pressureEstimate : \ref around1bar or \ref around155bars
26 * \param [in] int : mesh dimension
27 * \param [in] bool : There are two possible equations of state for the fluid
29 SinglePhase(phaseType fluid, pressureEstimate pEstimate,int dim,bool useDellacherieEOS=false);
32 * \brief sets the viscosity
33 * @param viscosite : value of the dynamic viscosity
35 void setViscosityConstant( double viscosite ){
36 _fluides[0]->setViscosity(viscosite);
39 //! system initialisation
42 //fonctions d'echange de flux
43 // void getOutputField(const Vec &Flux, const string Champ, const int numBord)=0;//, PetscInt *indices_Flux, PetscInt *indices_Bord, const long range)=0;
44 // double trace(const int &numBord, Vec &out)=0;
45 void testConservation();
49 /** \fn setIntletBoundaryCondition
50 * \brief adds a new boundary condition of type Inlet
52 * \param [in] string : the name of the boundary
53 * \param [in] double : the value of the temperature at the boundary
54 * \param [in] double : the value of the x component of the velocity at the boundary
55 * \param [in] double : the value of the y component of the velocity at the boundary
56 * \param [in] double : the value of the z component of the velocity at the boundary
59 void setInletBoundaryCondition(string groupName,double Temperature,double v_x=0, double v_y=0, double v_z=0){
60 _limitField[groupName]=LimitField(Inlet,-1,vector<double>(1,v_x),vector<double>(1,v_y),vector<double>(1,v_z),Temperature,-1,-1,-1);
62 /** \fn setIntletRotationBoundaryCondition
63 * \brief adds a new boundary condition of type InletRotationVelocity
65 * \param [in] string : the name of the boundary
66 * \param [in] double : the value of the temperature at the boundary
67 * \param [in] double : the components of the rotational of the inlet velocity
70 void setInletRotationBoundaryCondition(string groupName,double Temperature,double omega_x=0, double omega_y=0, double omega_z=0){
71 _limitField[groupName]=LimitField(InletRotationVelocity,0,vector<double>(1,omega_x),vector<double>(1,omega_y),vector<double>(1,omega_z),Temperature,-1,-1,-1);
73 /** \fn setIntletPressureBoundaryCondition
74 * \brief adds a new boundary condition of type InletPressure
76 * \param [in] string : the name of the boundary
77 * \param [in] double : the value of the pressure at the boundary
78 * \param [in] double : the value of the temperature at the boundary
79 * \param [in] double : the components of the rotational of the inlet velocity
82 void setInletPressureBoundaryCondition(string groupName, double pressure,double Temperature,double omega_x=0, double omega_y=0, double omega_z=0){
83 _limitField[groupName]=LimitField(InletPressure,pressure,vector<double>(1,omega_x),vector<double>(1,omega_y),vector<double>(1,omega_z),Temperature,-1,-1,-1);
85 /** \fn setIntletPressureBoundaryCondition
86 * \brief adds a new boundary condition of type InletPressure taking into account the hydrostatic pressure variations
87 * \details The pressure is not constant on the boundary but varies linearly with a slope given by the gravity vector
88 * \param [in] string : the name of the boundary
89 * \param [in] double : the value of the pressure at the boundary
90 * \param [in] double : the value of the temperature at the boundary
91 * \param [in] vector<double> : reference_point position on the boundary where the value Pressure will be imposed
94 void setInletPressureBoundaryCondition(string groupName, double pressure,double Temperature, vector<double> reference_point){
95 /* On the boundary we have P-Pref=rho g\cdot(x-xref) hence P=Pref-g\cdot xref + g\cdot x */
96 pressure-=reference_point[0]*_GravityField3d[0];
98 pressure-=reference_point[1]*_GravityField3d[1];
100 pressure-=reference_point[2]*_GravityField3d[2];
103 _limitField[groupName]=LimitField(InletPressure,pressure,vector<double>(0,0),vector<double>(0,0),vector<double>(0,0),Temperature,-1,-1,-1);
105 /** \fn setWallBoundaryCondition
106 * \brief adds a new boundary condition of type Wall
108 * \param [in] string : the name of the boundary
109 * \param [in] double : the value of the temperature at the boundary
110 * \param [in] double : the value of the x component of the velocity at the boundary
111 * \param [in] double : the value of the y component of the velocity at the boundary
112 * \param [in] double : the value of the z component of the velocity at the boundary
115 void setWallBoundaryCondition(string groupName,double Temperature=-1, double v_x=0, double v_y=0, double v_z=0){
117 _limitField[groupName]=LimitField(Wall,-1,vector<double>(1,v_x),vector<double>(1,v_y),vector<double>(1,v_z),Temperature,-1,-1,-1);
119 _limitField[groupName]=LimitField(Wall,-1,vector<double>(1,v_x),vector<double>(1,v_y),vector<double>(1,v_z),getReferenceTemperature(),-1,-1,-1);
122 /** \fn computeNewtonVariation
123 * \brief Builds and solves the linear system to obtain the variation Vkp1-Vk in a Newton scheme using primitive variables
126 void computeNewtonVariation();
128 /** \fn iterateTimeStep
129 * \brief calls computeNewtonVariation to perform one Newton iteration and tests the convergence
131 * @return boolean ok is true is the newton iteration gave a physically acceptable result
133 bool iterateTimeStep(bool &ok);
135 double getReferencePressure() { return _Pref; };
136 double getReferenceTemperature() { return _Tref; };
138 //get output fields for postprocessing or coupling
139 vector<string> getOutputFieldsNames() ;//liste tous les champs que peut fournir le code pour le postraitement
140 Field& getOutputField(const string& nameField );//Renvoie un champs pour le postraitement
141 Field& getPressureField();
142 Field& getVelocityField();
143 Field& getVelocityXField();
144 Field& getTemperatureField();
145 Field& getDensityField();
146 Field& getMomentumField();
147 Field& getTotalEnergyField();
148 Field& getEnthalpyField();
151 double _drho_sur_dp, _drho_sur_dT;//derivatives of the density rho wrt cv, p, T
152 double _drhoE_sur_dp, _drhoE_sur_dT;//derivatives of the total energy rho E wrt cv, p, T
153 bool _useDellacherieEOS;
154 double _Tref; //EOS reference temperature
155 double _Pref; //EOS reference pressure
157 //!calcule l'etat de Roe de deux etats
158 void convectionState( const long &i, const long &j, const bool &IsBord);
159 //!calcule la matrice de convection de l'etat interfacial entre deux cellules voisinnes
160 void convectionMatrices();
161 //!Calcule le flux pour un état et une porosité et une normale donnés
162 Vector convectionFlux(Vector U,Vector V, Vector normale, double porosity);
163 //!calcule la matrice de diffusion de l'etat interface pour la diffusion
164 void diffusionStateAndMatrices(const long &i,const long &j, const bool &IsBord);
165 //!Computes the source vector associated to the cell i
166 void sourceVector(PetscScalar * Si,PetscScalar * Ui,PetscScalar * Vi, int i);
167 //!Computes the pressure loss associated to the face ij
168 void pressureLossVector(PetscScalar * pressureLoss, double K, PetscScalar * Ui, PetscScalar * Vi, PetscScalar * Uj, PetscScalar * Vj);
169 //!Computes the contribution of the porosity gradient associated to the face ij to the source term
170 void porosityGradientSourceVector();
171 //!Calcule la jacobienne de la CL convection
172 void jacobian(const int &j, string nameOfGroup,double * normale);
173 //!Calcule la jacobienne de la CL de diffusion
174 void jacobianDiff(const int &j, string nameOfGroup);
175 //!Calcule l'etat fictif a la frontiere
176 void setBoundaryState(string nameOfGroup, const int &j,double *normale);// delete &nf Kieu
177 //!Adds the contribution of diffusion to the RHS
178 void addDiffusionToSecondMember(const int &i,const int &j,bool isBord);
179 //!Computation of the Roe matrix
180 void RoeMatrixConservativeVariables(double u_n, double total_enthalpy,Vector velocity, double k, double K);
181 void convectionMatrixPrimitiveVariables( double rho, double u_n, double H,Vector velocity);
182 //!Computation of the staggered Roe upwinding matrix in conservative variables
183 void staggeredRoeUpwindingMatrixConservativeVariables( double u_n, double total_enthalpy, Vector velocity, double k, double K);
184 //!Computation of the staggered Roe upwinding matrix in primitive variables
185 void staggeredRoeUpwindingMatrixPrimitiveVariables(double density, double u_n,double total_enthalpy, Vector velocity);
186 /**** staggered VFFC scheme has some specific features (no need for Roe matrix), hence some specific functions ******/
187 //!Computes the interfacial flux for the VFFC formulation of the staggered upwinding
188 Vector staggeredVFFCFlux();
189 //!Computes the matrices A^+ and A^- for the VFFC formulation of the staggered upwinding
190 void staggeredVFFCMatricesConservativeVariables(double u_n);
191 //!Computes the matrices A^+ and A^- for the VFFC formulation of the staggered upwinding using Primitive Variables
192 void staggeredVFFCMatricesPrimitiveVariables(double u_n);
193 //!Compute the corrected interfacial state for lowMach, pressureCorrection and staggered versions of the VFRoe formulation
194 void applyVFRoeLowMachCorrections(bool isBord, string groupname="");
195 //!Special preconditioner based on a matrix scaling strategy
196 void computeScaling(double offset);
197 //!Calcule les saut de valeurs propres pour la correction entropique
198 void entropicShift(double* n);
199 // Fonctions utilisant la loi d'etat
200 void consToPrim(const double *Ucons, double* Vprim,double porosity=1);
201 void primToCons(const double *V, const int &i, double *U, const int &j);
202 void primToConsJacobianMatrix(double *V);
203 /** \fn getDensityDerivatives
204 * \brief Computes the partial derivatives of rho, and rho E with regard to the primitive variables p and T
207 * @param square of the velocity vector
209 void getDensityDerivatives( double pressure, double temperature, double v2);
212 Field _Enthalpy, _Pressure, _Density, _Temperature, _Momentum, _TotalEnergy, _Vitesse, _VitesseX, _VitesseY, _VitesseZ;
215 #endif /* SINGLEPHASE_HXX_*/