Main class for defining the Navier-Stokes flow solver. More...
#include <solver_structure.hpp>
Inheritance diagram for CNSSolver:
Public Member Functions | |
| CNSSolver (void) | |
| Constructor of the class. | |
| CNSSolver (CGeometry *geometry, CConfig *config, unsigned short iMesh) | |
| ~CNSSolver (void) | |
| Destructor of the class. | |
| su2double | GetSurface_CL_Visc (unsigned short val_marker) |
| Provide the non dimensional lift coefficient. More... | |
| su2double | GetSurface_CD_Visc (unsigned short val_marker) |
| Provide the non dimensional drag coefficient. More... | |
| su2double | GetSurface_CSF_Visc (unsigned short val_marker) |
| Provide the non dimensional side-force coefficient. More... | |
| su2double | GetSurface_CEff_Visc (unsigned short val_marker) |
| Provide the non dimensional side-force coefficient. More... | |
| su2double | GetSurface_CFx_Visc (unsigned short val_marker) |
| Provide the non dimensional x force coefficient. More... | |
| su2double | GetSurface_CFy_Visc (unsigned short val_marker) |
| Provide the non dimensional y force coefficient. More... | |
| su2double | GetSurface_CFz_Visc (unsigned short val_marker) |
| Provide the non dimensional z force coefficient. More... | |
| su2double | GetSurface_CMx_Visc (unsigned short val_marker) |
| Provide the non dimensional x moment coefficient. More... | |
| su2double | GetSurface_CMy_Visc (unsigned short val_marker) |
| Provide the non dimensional y moment coefficient. More... | |
| su2double | GetSurface_CMz_Visc (unsigned short val_marker) |
| Provide the non dimensional z moment coefficient. More... | |
| su2double | GetAllBound_CL_Visc (void) |
| Get the inviscid contribution to the lift coefficient. More... | |
| su2double | GetAllBound_CD_Visc (void) |
| Get the inviscid contribution to the drag coefficient. More... | |
| su2double | GetAllBound_CSF_Visc (void) |
| Get the inviscid contribution to the sideforce coefficient. More... | |
| su2double | GetAllBound_CEff_Visc (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMx_Visc (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMy_Visc (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMz_Visc (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFx_Visc (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFy_Visc (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFz_Visc (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetViscosity_Inf (void) |
| Compute the viscosity at the infinity. More... | |
| su2double | GetTke_Inf (void) |
| Get the turbulent kinetic energy at the infinity. More... | |
| void | SetTime_Step (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned long Iteration) |
| Compute the time step for solving the Navier-Stokes equations with turbulence model. More... | |
| void | Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, unsigned short iRKStep, unsigned short RunTime_EqSystem, bool Output) |
| Restart residual and compute gradients. More... | |
| unsigned long | SetPrimitive_Variables (CSolver **solver_container, CConfig *config, bool Output) |
| Compute the velocity^2, SoundSpeed, Pressure, Enthalpy, Viscosity. More... | |
| void | BC_HeatFlux_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose a constant heat-flux condition at the wall. More... | |
| void | BC_Isothermal_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the Navier-Stokes boundary condition (strong). More... | |
| void | Friction_Forces (CGeometry *geometry, CConfig *config) |
| Compute the viscous forces and all the addimensional coefficients. More... | |
| su2double | GetSurface_HF_Visc (unsigned short val_marker) |
| Get the total heat flux. More... | |
| su2double | GetSurface_MaxHF_Visc (unsigned short val_marker) |
| Get the maximum (per surface) heat flux. More... | |
| su2double | GetCL_Visc (unsigned short val_marker) |
| Get the non dimensional lift coefficient (viscous contribution). More... | |
| su2double | GetCMz_Visc (unsigned short val_marker) |
| Get the non dimensional z moment coefficient (viscous contribution). More... | |
| su2double | GetCSF_Visc (unsigned short val_marker) |
| Get the non dimensional sideforce coefficient (viscous contribution). More... | |
| su2double | GetCD_Visc (unsigned short val_marker) |
| Get the non dimensional drag coefficient (viscous contribution). More... | |
| void | Viscous_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh, unsigned short iRKStep) |
| Compute the viscous residuals. More... | |
| su2double | GetCSkinFriction (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim) |
| Get the skin friction coefficient. More... | |
| su2double | GetHeatFlux (unsigned short val_marker, unsigned long val_vertex) |
| Get the skin friction coefficient. More... | |
| su2double | GetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex) |
| Get the skin friction coefficient. More... | |
| void | SetHeatFluxTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_heat) |
| Set the value of the target Pressure coefficient. More... | |
| su2double | GetYPlus (unsigned short val_marker, unsigned long val_vertex) |
| Get the y plus. More... | |
| su2double | GetOmega_Max (void) |
| Get the max Omega. More... | |
| su2double | GetStrainMag_Max (void) |
| Get the max Strain rate magnitude. More... | |
| void | SetStrainMag_Max (su2double val_strainmag_max) |
| A virtual member. More... | |
| void | SetOmega_Max (su2double val_omega_max) |
| A virtual member. More... | |
 Public Member Functions inherited from CEulerSolver | |
| CEulerSolver (void) | |
| Constructor of the class. | |
| CEulerSolver (CGeometry *geometry, CConfig *config, unsigned short iMesh) | |
| virtual | ~CEulerSolver (void) |
| Destructor of the class. | |
| void | Set_MPI_Solution (CGeometry *geometry, CConfig *config) |
| Impose the send-receive boundary condition. More... | |
| void | Set_MPI_Solution_Gradient (CGeometry *geometry, CConfig *config) |
| Impose the send-receive boundary condition. More... | |
| void | Set_MPI_Solution_Old (CGeometry *geometry, CConfig *config) |
| Impose the send-receive boundary condition. More... | |
| void | Set_MPI_Solution_Limiter (CGeometry *geometry, CConfig *config) |
| Impose the send-receive boundary condition. More... | |
| void | Set_MPI_Primitive_Limiter (CGeometry *geometry, CConfig *config) |
| Impose the send-receive boundary condition. More... | |
| void | SetNondimensionalization (CGeometry *geometry, CConfig *config, unsigned short iMesh) |
| Impose the send-receive boundary condition. More... | |
| CFluidModel * | GetFluidModel (void) |
| Compute the pressure at the infinity. More... | |
| su2double | GetDensity_Inf (void) |
| Compute the density at the infinity. More... | |
| su2double | GetModVelocity_Inf (void) |
| Compute 2-norm of the velocity at the infinity. More... | |
| su2double | GetDensity_Energy_Inf (void) |
| Compute the density multiply by energy at the infinity. More... | |
| su2double | GetPressure_Inf (void) |
| Compute the pressure at the infinity. More... | |
| su2double | GetDensity_Velocity_Inf (unsigned short val_dim) |
| Compute the density multiply by velocity at the infinity. More... | |
| su2double | GetVelocity_Inf (unsigned short val_dim) |
| Get the velocity at the infinity. More... | |
| su2double * | GetVelocity_Inf (void) |
| Get the velocity at the infinity. More... | |
| void | Centered_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh, unsigned short iRKStep) |
| Compute the spatial integration using a centered scheme. More... | |
| void | Upwind_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh) |
| Compute the spatial integration using a upwind scheme. More... | |
| void | ComputeConsExtrapolation (CConfig *config) |
| Compute the extrapolated quantities, for MUSCL upwind 2nd reconstruction, in a more thermodynamic consistent way. More... | |
| void | Source_Residual (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CNumerics *second_numerics, CConfig *config, unsigned short iMesh) |
| Source term integration. More... | |
| void | Source_Template (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short iMesh) |
| Source term integration. More... | |
| void | Postprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh) |
| A virtual member. More... | |
| void | SetDissipation_Switch (CGeometry *geometry, CConfig *config) |
| Compute a pressure sensor switch. More... | |
| void | Set_MPI_Dissipation_Switch (CGeometry *geometry, CConfig *config) |
| Parallelization of SetDissipation_Switch. More... | |
| void | SetPrimitive_Gradient_GG (CGeometry *geometry, CConfig *config) |
| Compute the gradient of the primitive variables using Green-Gauss method, and stores the result in the Gradient_Primitive variable. More... | |
| void | SetPrimitive_Gradient_LS (CGeometry *geometry, CConfig *config) |
| Compute the gradient of the primitive variables using a Least-Squares method, and stores the result in the Gradient_Primitive variable. More... | |
| void | Set_MPI_Primitive_Gradient (CGeometry *geometry, CConfig *config) |
| Compute the gradient of the primitive variables using Green-Gauss method, and stores the result in the Gradient_Primitive variable. More... | |
| void | SetPrimitive_Limiter (CGeometry *geometry, CConfig *config) |
| Compute the limiter of the primitive variables. More... | |
| void | SetPreconditioner (CConfig *config, unsigned long iPoint) |
| Compute the gradient of the primitive variables using a Least-Squares method, and stores the result in the Gradient_Primitive variable. More... | |
| void | SetUndivided_Laplacian (CGeometry *geometry, CConfig *config) |
| Compute the undivided laplacian for the solution, except the energy equation. More... | |
| void | Set_MPI_Undivided_Laplacian (CGeometry *geometry, CConfig *config) |
| Parallelization of Undivided Laplacian. More... | |
| void | SetMax_Eigenvalue (CGeometry *geometry, CConfig *config) |
| Compute the max eigenvalue. More... | |
| void | Set_MPI_MaxEigenvalue (CGeometry *geometry, CConfig *config) |
| Parallelization of the Max eigenvalue. More... | |
| void | Set_MPI_ActDisk (CSolver **solver_container, CGeometry *geometry, CConfig *config) |
| Parallelization of Undivided Laplacian. More... | |
| void | Set_MPI_Nearfield (CGeometry *geometry, CConfig *config) |
| Parallelization of Undivided Laplacian. More... | |
| void | Set_MPI_Interface (CGeometry *geometry, CConfig *config) |
| Parallelization of Undivided Laplacian. More... | |
| void | Compute_ComboObj (CConfig *config) |
| Compute weighted-sum "combo" objective output. More... | |
| void | BC_Euler_Wall (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| Impose via the residual the Euler wall boundary condition. More... | |
| void | BC_Far_Field (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the far-field boundary condition using characteristics. More... | |
| void | BC_Sym_Plane (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the symmetry boundary condition using the residual. More... | |
| void | BC_Fluid_Interface (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config) |
| Impose the interface state across sliding meshes. More... | |
| void | BC_ActDisk_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the engine inflow boundary condition. More... | |
| void | BC_ActDisk_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the engine exhaust boundary condition. More... | |
| void | BC_ActDisk (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker, bool inlet_surface) |
| Impose the engine inflow boundary condition. More... | |
| void | BC_Interface_Boundary (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| Impose the interface boundary condition using the residual. More... | |
| void | BC_NearField_Boundary (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| Impose the near-field boundary condition using the residual. More... | |
| void | BC_Dirichlet (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short val_marker) |
| Impose the dirichlet boundary condition using the residual. More... | |
| void | BC_Riemann (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the boundary condition using characteristic recostruction. More... | |
| void | BC_NonReflecting (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the boundary condition using characteristic recostruction. More... | |
| void | BC_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose a subsonic inlet boundary condition. More... | |
| void | BC_Supersonic_Inlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose a supersonic inlet boundary condition. More... | |
| void | BC_Supersonic_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose a supersonic outlet boundary condition. More... | |
| void | BC_Custom (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| Impose the dirichlet boundary condition. More... | |
| void | BC_Outlet (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the outlet boundary condition. More... | |
| void | BC_Engine_Inflow (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the nacelle inflow boundary condition. More... | |
| void | BC_Engine_Exhaust (CGeometry *geometry, CSolver **solver_container, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short val_marker) |
| Impose the ancelle exhaust boundary condition. More... | |
| void | Mixing_Process (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short val_Marker) |
| It avarage the fluxes value along a boundary. More... | |
| void | MixedOut_Average (su2double val_init_pressure, su2double *val_Averaged_Flux, su2double *val_normal, su2double *pressure_mix, su2double *density_mix) |
| it performs a mixed out average of the nodes of a boundary. More... | |
| void | MixedOut_Root_Function (su2double *pressure, su2double *val_Averaged_Flux, su2double *val_normal, su2double *valfunc, su2double *density) |
| it finds the root of an implicit equation that relates pressure and density. More... | |
| void | Boundary_Fourier (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short val_Marker, vector< std::complex< su2double > > &c4k, signed long &nboundaryvertex) |
| it performs a fourier transformation of a characteristic value. More... | |
| void | Boundary_Fourier (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short val_Marker, vector< std::complex< su2double > > &c2k, vector< std::complex< su2double > > &c3k, signed long &nboundaryvertex) |
| it performs a fourier transformation of a characteristic value. More... | |
| void | SetExtAveragedValue (CSolver *solver_container, unsigned short intMarker, unsigned short extMarker) |
| A virtual member. More... | |
| su2double | GetAveragedDensity (unsigned short valMarker) |
| Provide the average density at the boundary of interest. More... | |
| su2double | GetAveragedTotPressure (unsigned short valMarker) |
| Provide the average pressure at the boundary of interest. More... | |
| su2double | GetTotalPressureLoss (unsigned short inMarkerTP) |
| Provide Total Pressure Losses (turbomachinery performance). More... | |
| su2double | GetKineticEnergyLoss (unsigned short inMarkerTP) |
| Provide Kinetic Energy Losses (turbomachinery performance). More... | |
| su2double | GetTotalTotalEfficiency (unsigned short inMarkerTP) |
| Provide Total-Total Efficiency (turbomachinery performance). More... | |
| su2double | GetTotalStaticEfficiency (unsigned short inMarkerTP) |
| Provide Total-Static Efficiency (turbomachinery performance). More... | |
| su2double | GetEulerianWork (unsigned short inMarkerTP) |
| Provide the Eulerian Work (turbomachinery performance). More... | |
| su2double | GetTotalEnthalpyIn (unsigned short inMarkerTP) |
| Provide the Inlet Total Enthalpy (turbomachinery performance). More... | |
| su2double | GetFlowAngleIn (unsigned short inMarkerTP) |
| Provide the Inlet Flow Angle (turbomachinery performance). More... | |
| su2double | GetFlowAngleOut (unsigned short inMarkerTP) |
| Provide the Outlet Flow Angle (turbomachinery performance). More... | |
| su2double | GetMassFlowIn (unsigned short inMarkerTP) |
| Provide the Inlet Mass Flow (turbomachinery performance). More... | |
| su2double | GetMassFlowOut (unsigned short inMarkerTP) |
| Provide the Outlet Mass Flow (turbomachinery performance). More... | |
| su2double | GetMachIn (unsigned short inMarkerTP) |
| Provide the Inlet Mach number (turbomachinery performance). More... | |
| su2double | GetMachOut (unsigned short inMarkerTP) |
| Provide the Outlet Mach number (turbomachinery performance). More... | |
| su2double | GetNormalMachIn (unsigned short inMarkerTP) |
| Provide the normal component of the Inlet Mach number (turbomachinery performance). More... | |
| su2double | GetNormalMachOut (unsigned short inMarkerTP) |
| Provide the normal component of the Outlet Mach number (turbomachinery performance). More... | |
| su2double | GetEnthalpyOut (unsigned short inMarkerTP) |
| Provide the Outlet Enthalpy (turbomachinery performance). More... | |
| su2double | GetVelocityOutIs (unsigned short inMarkerTP) |
| Provide the Isentropic Outlet Velocity (turbomachinery performance). More... | |
| su2double | GetPressureOut (unsigned short inMarkerTP) |
| Provide the Outlet Pressure (turbomachinery performance). More... | |
| su2double | GetPressureRatio (unsigned short inMarkerTP) |
| Provide Pressure Ratio (tubomachinery performance). More... | |
| su2double | GetAveragedTotTemperature (unsigned short valMarker) |
| Provide Averaged Total Temperature at the boundary of interest. More... | |
| su2double | GetAveragedPressure (unsigned short valMarker) |
| Provide the Average pressure at the boundary of interest. More... | |
| su2double | GetMassFlow (unsigned short valMarker) |
| Provide the MassFlow at the boundary of interest. More... | |
| su2double | GetFlowAngle (unsigned short valMarker) |
| Provide the Flow Angle at the boundary of interest. More... | |
| su2double | GetAveragedMach (unsigned short valMarker) |
| Provide the Mach number at the boundary of interest. More... | |
| su2double | GetAveragedNormalMach (unsigned short valMarker) |
| Provide the Normal Mach number at the boundary of interest. More... | |
| su2double | GetAveragedEnthalpy (unsigned short valMarker) |
| Provide the average enthalpy at the boundary of interest. More... | |
| su2double | GetAveragedEntropy (unsigned short valMarker) |
| Provide the average pressure at the boundary of interest. More... | |
| su2double * | GetAveragedVelocity (unsigned short valMarker) |
| Provide the average pressure at the boundary of interest. More... | |
| su2double * | GetAveragedGridVelocity (unsigned short valMarker) |
| Provide the average grid velocity at the boundary of interest. More... | |
| su2double | GetAveragedNormalVelocity (unsigned short valMarker) |
| Provide the Average Normal Velocity at the boundary of interest. More... | |
| su2double | GetAveragedTangVelocity (unsigned short valMarker) |
| Provide the Tangent Velocity at the boundary of interest. More... | |
| void | ExplicitRK_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep) |
| Update the solution using a Runge-Kutta scheme. More... | |
| void | GetSurface_Properties (CGeometry *geometry, CNumerics *conv_numerics, CNumerics *visc_numerics, CConfig *config, unsigned short iMesh, bool Output) |
| Compute the Fan face Mach number. More... | |
| void | GetPower_Properties (CGeometry *geometry, CConfig *config, unsigned short iMesh, bool Output) |
| Compute the Fan face Mach number. More... | |
| void | GetSurface_Distortion (CGeometry *geometry, CConfig *config, unsigned short iMesh, bool Output) |
| Compute the Fan face Mach number. More... | |
| void | SetActDisk_BCThrust (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output) |
| Update the AoA and freestream velocity at the farfield. More... | |
| void | SetFarfield_AoA (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh, bool Output) |
| Update the AoA and freestream velocity at the farfield. More... | |
| void | ExplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| Update the solution using the explicit Euler scheme. More... | |
| void | ImplicitEuler_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| Update the solution using an implicit Euler scheme. More... | |
| void | Pressure_Forces (CGeometry *geometry, CConfig *config) |
| Compute the pressure forces and all the adimensional coefficients. More... | |
| void | Momentum_Forces (CGeometry *geometry, CConfig *config) |
| Compute the pressure forces and all the adimensional coefficients. More... | |
| void | TurboPerformance (CSolver *solver, CConfig *config, unsigned short inMarker, unsigned short outMarker, unsigned short Kind_TurboPerf, unsigned short inMarkerTP) |
| Compute turbomachinery performance. More... | |
| void | StoreTurboPerformance (CSolver *solver, unsigned short inMarkerTP) |
| Compute turbomachinery performance. More... | |
| su2double | GetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state) |
| Get the outer state for fluid interface nodes. More... | |
| su2double | GetCL_Inv (unsigned short val_marker) |
| Provide the non dimensional lift coefficient (inviscid contribution). More... | |
| su2double | GetCMz_Inv (unsigned short val_marker) |
| Provide the non dimensional z moment coefficient (inviscid contribution). More... | |
| su2double | GetSurface_CL (unsigned short val_marker) |
| Provide the non dimensional lift coefficient. More... | |
| su2double | GetSurface_CD (unsigned short val_marker) |
| Provide the non dimensional drag coefficient. More... | |
| su2double | GetSurface_CSF (unsigned short val_marker) |
| Provide the non dimensional side-force coefficient. More... | |
| su2double | GetSurface_CEff (unsigned short val_marker) |
| Provide the non dimensional side-force coefficient. More... | |
| su2double | GetSurface_CFx (unsigned short val_marker) |
| Provide the non dimensional x force coefficient. More... | |
| su2double | GetSurface_CFy (unsigned short val_marker) |
| Provide the non dimensional y force coefficient. More... | |
| su2double | GetSurface_CFz (unsigned short val_marker) |
| Provide the non dimensional z force coefficient. More... | |
| su2double | GetSurface_CMx (unsigned short val_marker) |
| Provide the non dimensional x moment coefficient. More... | |
| su2double | GetSurface_CMy (unsigned short val_marker) |
| Provide the non dimensional y moment coefficient. More... | |
| su2double | GetSurface_CMz (unsigned short val_marker) |
| Provide the non dimensional z moment coefficient. More... | |
| su2double | GetSurface_CL_Inv (unsigned short val_marker) |
| Provide the non dimensional lift coefficient. More... | |
| su2double | GetSurface_CD_Inv (unsigned short val_marker) |
| Provide the non dimensional drag coefficient. More... | |
| su2double | GetSurface_CSF_Inv (unsigned short val_marker) |
| Provide the non dimensional side-force coefficient. More... | |
| su2double | GetSurface_CEff_Inv (unsigned short val_marker) |
| Provide the non dimensional side-force coefficient. More... | |
| su2double | GetSurface_CFx_Inv (unsigned short val_marker) |
| Provide the non dimensional x force coefficient. More... | |
| su2double | GetSurface_CFy_Inv (unsigned short val_marker) |
| Provide the non dimensional y force coefficient. More... | |
| su2double | GetSurface_CFz_Inv (unsigned short val_marker) |
| Provide the non dimensional z force coefficient. More... | |
| su2double | GetSurface_CMx_Inv (unsigned short val_marker) |
| Provide the non dimensional x moment coefficient. More... | |
| su2double | GetSurface_CMy_Inv (unsigned short val_marker) |
| Provide the non dimensional y moment coefficient. More... | |
| su2double | GetSurface_CMz_Inv (unsigned short val_marker) |
| Provide the non dimensional z moment coefficient. More... | |
| su2double | GetSurface_CL_Mnt (unsigned short val_marker) |
| Provide the non dimensional lift coefficient. More... | |
| su2double | GetSurface_CD_Mnt (unsigned short val_marker) |
| Provide the non dimensional drag coefficient. More... | |
| su2double | GetSurface_CSF_Mnt (unsigned short val_marker) |
| Provide the non dimensional side-force coefficient. More... | |
| su2double | GetSurface_CEff_Mnt (unsigned short val_marker) |
| Provide the non dimensional side-force coefficient. More... | |
| su2double | GetSurface_CFx_Mnt (unsigned short val_marker) |
| Provide the non dimensional x force coefficient. More... | |
| su2double | GetSurface_CFy_Mnt (unsigned short val_marker) |
| Provide the non dimensional y force coefficient. More... | |
| su2double | GetSurface_CFz_Mnt (unsigned short val_marker) |
| Provide the non dimensional z force coefficient. More... | |
| su2double | GetSurface_CMx_Mnt (unsigned short val_marker) |
| Provide the non dimensional x moment coefficient. More... | |
| su2double | GetSurface_CMy_Mnt (unsigned short val_marker) |
| Provide the non dimensional y moment coefficient. More... | |
| su2double | GetSurface_CMz_Mnt (unsigned short val_marker) |
| Provide the non dimensional z moment coefficient. More... | |
| su2double | GetCD_Inv (unsigned short val_marker) |
| Provide the non dimensional drag coefficient (inviscid contribution). More... | |
| su2double | GetInflow_MassFlow (unsigned short val_marker) |
| Provide the mass flow rate. More... | |
| su2double | GetExhaust_MassFlow (unsigned short val_marker) |
| Provide the mass flow rate. More... | |
| su2double | GetInflow_Pressure (unsigned short val_marker) |
| Provide the mass flow rate. More... | |
| su2double | GetInflow_Mach (unsigned short val_marker) |
| Provide the mass flow rate. More... | |
| su2double | GetCSF_Inv (unsigned short val_marker) |
| Provide the non dimensional sideforce coefficient (inviscid contribution). More... | |
| su2double | GetCEff_Inv (unsigned short val_marker) |
| Provide the non dimensional efficiency coefficient (inviscid contribution). More... | |
| su2double | GetTotal_CSF (void) |
| Provide the total (inviscid + viscous) non dimensional sideforce coefficient. More... | |
| su2double | GetTotal_CEff (void) |
| Provide the total (inviscid + viscous) non dimensional efficiency coefficient. More... | |
| su2double | GetTotal_CEquivArea (void) |
| Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient. More... | |
| su2double | GetTotal_AeroCD (void) |
| Provide the total (inviscid + viscous) non dimensional aero CD. More... | |
| su2double | GetTotal_RadialDistortion (void) |
| Provide the total (inviscid + viscous) non dimensional fan face distortion. More... | |
| su2double | GetTotal_CircumferentialDistortion (void) |
| Provide the total (inviscid + viscous) non dimensional fan face distortion. More... | |
| su2double | GetTotal_CpDiff (void) |
| Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient. More... | |
| su2double | GetTotal_HeatFluxDiff (void) |
| Provide the total (inviscid + viscous) non dimensional Equivalent Area coefficient. More... | |
| su2double | GetTotal_CNearFieldOF (void) |
| Provide the total (inviscid + viscous) non dimensional Near-Field pressure coefficient. More... | |
| void | AddTotal_ComboObj (su2double val_obj) |
| Add to the value of the total 'combo' objective. More... | |
| void | SetTotal_CEquivArea (su2double val_cequivarea) |
| Set the value of the Equivalent Area coefficient. More... | |
| void | SetTotal_AeroCD (su2double val_aerocd) |
| Set the value of the Aero drag. More... | |
| void | SetTotal_RadialDistortion (su2double val_distortion) |
| Set the value of the fan face distortion. More... | |
| void | SetTotal_CircumferentialDistortion (su2double val_distortion) |
| Set the value of the fan face distortion. More... | |
| void | SetTotal_CpDiff (su2double val_pressure) |
| Set the value of the Equivalent Area coefficient. More... | |
| void | SetTotal_HeatFluxDiff (su2double val_heat) |
| Set the value of the Equivalent Area coefficient. More... | |
| void | SetTotal_CNearFieldOF (su2double val_cnearfieldpress) |
| Set the value of the Near-Field pressure oefficient. More... | |
| void | SetTotal_ComboObj (su2double ComboObj) |
| Set the total "combo" objective (weighted sum of other values). More... | |
| su2double | GetTotal_ComboObj (void) |
| Provide the total "combo" objective (weighted sum of other values). More... | |
| su2double | GetTotal_CL (void) |
| Provide the total (inviscid + viscous) non dimensional lift coefficient. More... | |
| su2double | GetTotal_CD (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_NetCThrust (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_Power (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_CD_SolidSurf (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_ReverseFlow (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_MFR (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_Prop_Eff (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_ByPassProp_Eff (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_Adiab_Eff (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_Poly_Eff (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_IDC (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_IDC_Mach (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_IDR (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_DC60 (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_Custom (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetTotal_CMx (void) |
| Provide the total (inviscid + viscous) non dimensional x moment coefficient. More... | |
| su2double | GetTotal_CMy (void) |
| Provide the total (inviscid + viscous) non dimensional y moment coefficient. More... | |
| su2double | GetTotal_CMz (void) |
| Provide the total (inviscid + viscous) non dimensional z moment coefficient. More... | |
| su2double | GetTotal_CFx (void) |
| Provide the total (inviscid + viscous) non dimensional x force coefficient. More... | |
| su2double | GetTotal_CFy (void) |
| Provide the total (inviscid + viscous) non dimensional y force coefficient. More... | |
| su2double | GetTotal_CFz (void) |
| Provide the total (inviscid + viscous) non dimensional z force coefficient. More... | |
| su2double | GetTotal_CT (void) |
| Provide the total (inviscid + viscous) non dimensional thrust coefficient. More... | |
| void | SetTotal_CT (su2double val_Total_CT) |
| Store the total (inviscid + viscous) non dimensional thrust coefficient. More... | |
| su2double | GetTotal_CQ (void) |
| Provide the total (inviscid + viscous) non dimensional torque coefficient. More... | |
| su2double | GetTotal_HeatFlux (void) |
| Provide the total heat load. More... | |
| su2double | GetTotal_MaxHeatFlux (void) |
| Provide the total heat load. More... | |
| void | SetTotal_CQ (su2double val_Total_CQ) |
| Store the total (inviscid + viscous) non dimensional torque coefficient. More... | |
| void | SetTotal_HeatFlux (su2double val_Total_Heat) |
| Store the total heat load. More... | |
| void | SetTotal_MaxHeatFlux (su2double val_Total_MaxHeat) |
| Store the total heat load. More... | |
| su2double | GetTotal_CMerit (void) |
| Provide the total (inviscid + viscous) non dimensional rotor Figure of Merit. More... | |
| void | SetTotal_CD (su2double val_Total_CD) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_CL (su2double val_Total_CL) |
| Store the total (inviscid + viscous) non dimensional lift coefficient. More... | |
| void | SetTotal_NetCThrust (su2double val_Total_NetCThrust) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_Power (su2double val_Total_Power) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_CD_SolidSurf (su2double val_Total_CD_SolidSurf) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_ReverseFlow (su2double val_ReverseFlow) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_MFR (su2double val_Total_MFR) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_Prop_Eff (su2double val_Total_Prop_Eff) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_ByPassProp_Eff (su2double val_Total_ByPassProp_Eff) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_Adiab_Eff (su2double val_Total_Adiab_Eff) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_Poly_Eff (su2double val_Total_Poly_Eff) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_IDC (su2double val_Total_IDC) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_IDC_Mach (su2double val_Total_IDC_Mach) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_IDR (su2double val_Total_IDR) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_DC60 (su2double val_Total_DC60) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | SetTotal_Custom (su2double val_Total_Custom, su2double val_coeff) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| void | AddTotal_Custom (su2double val_Total_Custom, su2double val_coeff) |
| Store the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| su2double | GetAllBound_CL_Inv (void) |
| Get the inviscid contribution to the lift coefficient. More... | |
| su2double | GetAllBound_CD_Inv (void) |
| Get the inviscid contribution to the drag coefficient. More... | |
| su2double | GetAllBound_CSF_Inv (void) |
| Get the inviscid contribution to the sideforce coefficient. More... | |
| su2double | GetAllBound_CEff_Inv (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMx_Inv (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMy_Inv (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMz_Inv (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFx_Inv (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFy_Inv (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFz_Inv (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CL_Mnt (void) |
| Get the inviscid contribution to the lift coefficient. More... | |
| su2double | GetAllBound_CD_Mnt (void) |
| Get the inviscid contribution to the drag coefficient. More... | |
| su2double | GetAllBound_CSF_Mnt (void) |
| Get the inviscid contribution to the sideforce coefficient. More... | |
| su2double | GetAllBound_CEff_Mnt (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMx_Mnt (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMy_Mnt (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CMz_Mnt (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFx_Mnt (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFy_Mnt (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetAllBound_CFz_Mnt (void) |
| Get the inviscid contribution to the efficiency coefficient. More... | |
| su2double | GetCPressure (unsigned short val_marker, unsigned long val_vertex) |
| Provide the Pressure coefficient. More... | |
| su2double | GetCPressureTarget (unsigned short val_marker, unsigned long val_vertex) |
| Provide the Target Pressure coefficient. More... | |
| void | SetCPressureTarget (unsigned short val_marker, unsigned long val_vertex, su2double val_pressure) |
| Set the value of the target Pressure coefficient. More... | |
| su2double * | GetCharacPrimVar (unsigned short val_marker, unsigned long val_vertex) |
| Value of the characteristic variables at the boundaries. More... | |
| void | SetCharacPrimVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var, su2double val_value) |
| Value of the characteristic variables at the boundaries. More... | |
| su2double * | GetDonorPrimVar (unsigned short val_marker, unsigned long val_vertex) |
| Value of the characteristic variables at the boundaries. More... | |
| void | SetDonorPrimVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var, su2double val_value) |
| Value of the characteristic variables at the boundaries. More... | |
| su2double | GetDonorPrimVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var) |
| Value of the characteristic variables at the boundaries. More... | |
| unsigned long | GetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex) |
| Value of the characteristic global index at the boundaries. More... | |
| void | SetDonorGlobalIndex (unsigned short val_marker, unsigned long val_vertex, unsigned long val_index) |
| Value of the characteristic global index at the boundaries. More... | |
| su2double | GetActDisk_DeltaP (unsigned short val_marker, unsigned long val_vertex) |
| Value of the characteristic global index at the boundaries. More... | |
| void | SetActDisk_DeltaP (unsigned short val_marker, unsigned long val_vertex, su2double val_deltap) |
| Value of the characteristic global index at the boundaries. More... | |
| su2double | GetActDisk_DeltaT (unsigned short val_marker, unsigned long val_vertex) |
| Value of the characteristic global index at the boundaries. More... | |
| void | SetActDisk_DeltaT (unsigned short val_marker, unsigned long val_vertex, su2double val_deltat) |
| Value of the characteristic global index at the boundaries. More... | |
| su2double | GetInlet_Ttotal (unsigned short val_marker, unsigned long val_vertex) |
| Value of the characteristic global index at the boundaries. More... | |
| su2double | GetInlet_Ptotal (unsigned short val_marker, unsigned long val_vertex) |
| Value of the characteristic global index at the boundaries. More... | |
| su2double | GetInlet_FlowDir (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim) |
| Value of the characteristic global index at the boundaries. More... | |
| void | SetInlet_Ttotal (unsigned short val_marker, unsigned long val_vertex, su2double val_ttotal) |
| Value of the characteristic global index at the boundaries. More... | |
| void | SetInlet_Ptotal (unsigned short val_marker, unsigned long val_vertex, su2double val_ptotal) |
| Value of the characteristic global index at the boundaries. More... | |
| void | SetInlet_FlowDir (unsigned short val_marker, unsigned long val_vertex, unsigned short val_dim, su2double val_flowdir) |
| Value of the characteristic global index at the boundaries. More... | |
| su2double | GetOneD_TotalPress (void) |
| Provide the averaged total pressure at a marker. | |
| void | SetOneD_TotalPress (su2double AveragePressure) |
| Set the value of averaged total pressure. More... | |
| su2double | GetOneD_Mach (void) |
| Provide the averaged Mach number at a marker. | |
| void | SetOneD_Mach (su2double AverageMach) |
| Set the averaged Mach number at a marker. | |
| su2double | GetOneD_Temp (void) |
| Provide the averaged Temperature number at a marker. | |
| void | SetOneD_Temp (su2double AverageTemperature) |
| Set the averaged Temperature at a marker. | |
| su2double | GetOneD_MassFlowRate (void) |
| Provide the averaged mass flow rate at a marker. | |
| void | SetOneD_MassFlowRate (su2double MassFlowRate) |
| Set the averaged mass flow rate at a marker. | |
| su2double | GetOneD_FluxAvgPress (void) |
| Get the flux averaged pressure at a marker.(same as area averaged pressure) | |
| void | SetOneD_FluxAvgPress (su2double PressureRef) |
| Set the flux averaged pressure at a marker. (same as area averaged pressure) | |
| su2double | GetOneD_FluxAvgDensity (void) |
| Get the flux averaged density at a marker. ( = (gamma/(gamma-1)) / ( Pref*(href-1/2 uref^2) ) | |
| void | SetOneD_FluxAvgDensity (su2double DensityRef) |
| Set the flux averaged density at a marker.( = (gamma/(gamma-1)) / ( Pref*(href-1/2 uref^2) ) | |
| su2double | GetOneD_FluxAvgVelocity (void) |
| Get the flux averaged velocity at a marker. = \( \sqrt ( \int((rho*u)*u^2dA)/\int(rho*u*dA) )\). | |
| void | SetOneD_FluxAvgVelocity (su2double VelocityRef) |
| Set the flux averaged velocity at a marker. = \( sqrt ( \int((rho*u)*u^2dA)/\int(rho*u*dA) ) \). | |
| su2double | GetOneD_FluxAvgEntalpy (void) |
| Get the flux averaged enthalpy at a marker. = \( \int(rho*u*h dA) / \int(rho *u *dA ) \). | |
| void | SetOneD_FluxAvgEntalpy (su2double EnthalpyRef) |
| Set the flux averaged enthalpy at a marker. = \( \int(rho*u*h dA) / \int(rho *u *dA ) \). | |
| void | SetResidual_DualTime (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iRKStep, unsigned short iMesh, unsigned short RunTime_EqSystem) |
| Set the total residual adding the term that comes from the Dual Time Strategy. More... | |
| void | SetFlow_Displacement (CGeometry **flow_geometry, CVolumetricMovement *flow_grid_movement, CConfig *flow_config, CConfig *fea_config, CGeometry **fea_geometry, CSolver ***fea_solution) |
| A virtual member. More... | |
| void | SetFlow_Displacement_Int (CGeometry **flow_geometry, CVolumetricMovement *flow_grid_movement, CConfig *flow_config, CConfig *fea_config, CGeometry **fea_geometry, CSolver ***fea_solution) |
| A virtual member. More... | |
| void | LoadRestart (CGeometry **geometry, CSolver ***solver, CConfig *config, int val_iter) |
| Load a solution from a restart file. More... | |
| void | SetSlidingState (unsigned short val_marker, unsigned long val_vertex, unsigned short val_state, su2double component) |
| Set the outer state for fluid interface nodes. More... | |
| void | SetInitialCondition (CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long ExtIter) |
| Set the initial condition for the Euler Equations. More... | |
| void | SetPressure_Inf (su2double p_inf) |
| Set the freestream pressure. More... | |
| void | SetTemperature_Inf (su2double t_inf) |
| Set the freestream temperature. More... | |
| void | SetFreeStream_Solution (CConfig *config) |
| Set the solution using the Freestream values. More... | |
| Public Member Functions inherited from CSolver | |
| CSolver (void) | |
| Constructor of the class. | |
| virtual | ~CSolver (void) |
| Destructor of the class. | |
| void | SetIterLinSolver (unsigned short val_iterlinsolver) |
| Set number of linear solver iterations. More... | |
| virtual void | Set_MPI_Primitive (CGeometry *geometry, CConfig *config) |
| Set number of linear solver iterations. More... | |
| void | SetResidual_RMS (CGeometry *geometry, CConfig *config) |
| Set number of linear solver iterations. More... | |
| virtual void | Set_MPI_Solution_DispOnly (CGeometry *geometry, CConfig *config) |
| Impose the send-receive boundary condition for velocities and accelerations in structural solutions. More... | |
| virtual void | Set_MPI_Solution_Pred (CGeometry *geometry, CConfig *config) |
| Impose the send-receive boundary condition for predicted FSI structural solutions. More... | |
| virtual void | Set_MPI_Solution_Pred_Old (CGeometry *geometry, CConfig *config) |
| Impose the send-receive boundary condition for old predicted FSI structural solutions. More... | |
| unsigned short | GetIterLinSolver (void) |
| Get number of linear solver iterations. More... | |
| su2double | GetMax_Delta_Time (void) |
| Get the value of the maximum delta time. More... | |
| su2double | GetMin_Delta_Time (void) |
| Get the value of the minimum delta time. More... | |
| virtual su2double | GetMax_Delta_Time (unsigned short val_Species) |
| Get the value of the maximum delta time. More... | |
| virtual su2double | GetMin_Delta_Time (unsigned short val_Species) |
| Get the value of the minimum delta time. More... | |
| unsigned short | GetnVar (void) |
| Get the number of variables of the problem. | |
| unsigned short | GetnPrimVar (void) |
| Get the number of variables of the problem. | |
| unsigned short | GetnPrimVarGrad (void) |
| Get the number of variables of the problem. | |
| unsigned short | GetnSecondaryVar (void) |
| Get the number of variables of the problem. | |
| unsigned short | GetnSecondaryVarGrad (void) |
| Get the number of variables of the problem. | |
| unsigned short | GetnOutputVariables (void) |
| Get the number of variables of the problem. | |
| void | SetRes_RMS (unsigned short val_var, su2double val_residual) |
| Set the maximal residual, this is useful for the convergence history. More... | |
| void | AddRes_RMS (unsigned short val_var, su2double val_residual) |
| Adds the maximal residual, this is useful for the convergence history. More... | |
| su2double | GetRes_RMS (unsigned short val_var) |
| Get the maximal residual, this is useful for the convergence history. More... | |
| void | SetRes_Max (unsigned short val_var, su2double val_residual, unsigned long val_point) |
| Set the maximal residual, this is useful for the convergence history. More... | |
| void | AddRes_Max (unsigned short val_var, su2double val_residual, unsigned long val_point, su2double *val_coord) |
| Adds the maximal residual, this is useful for the convergence history. More... | |
| su2double | GetRes_Max (unsigned short val_var) |
| Get the maximal residual, this is useful for the convergence history. More... | |
| virtual su2double | GetRes_FEM (unsigned short val_var) |
| Get the residual for FEM structural analysis. More... | |
| unsigned long | GetPoint_Max (unsigned short val_var) |
| Get the maximal residual, this is useful for the convergence history. More... | |
| su2double * | GetPoint_Max_Coord (unsigned short val_var) |
| Get the location of the maximal residual, this is useful for the convergence history. More... | |
| void | SetGrid_Movement_Residual (CGeometry *geometry, CConfig *config) |
| Set Value of the residual if there is a grid movement. More... | |
| void | SetAuxVar_Gradient_GG (CGeometry *geometry, CConfig *config) |
| Compute the Green-Gauss gradient of the auxiliary variable. More... | |
| void | SetAuxVar_Gradient_LS (CGeometry *geometry, CConfig *config) |
| Compute the Least Squares gradient of the auxiliary variable. More... | |
| void | SetAuxVar_Surface_Gradient (CGeometry *geometry, CConfig *config) |
| Compute the Least Squares gradient of an auxiliar variable on the profile surface. More... | |
| void | SetSolution_Gradient_GG (CGeometry *geometry, CConfig *config) |
| Compute the Green-Gauss gradient of the solution. More... | |
| void | SetSolution_Gradient_LS (CGeometry *geometry, CConfig *config) |
| Compute the Least Squares gradient of the solution. More... | |
| void | SetGridVel_Gradient (CGeometry *geometry, CConfig *config) |
| Compute the Least Squares gradient of the grid velocity. More... | |
| void | SetSolution_Limiter (CGeometry *geometry, CConfig *config) |
| Compute slope limiter. More... | |
| void | SetPressureLaplacian (CGeometry *geometry, CConfig *config, su2double *PressureLaplacian) |
| A virtual member. More... | |
| void | Set_OldSolution (CGeometry *geometry) |
| Set the old solution variables to the current solution value for Runge-Kutta iteration. More... | |
| void | Restart_OldGeometry (CGeometry *geometry, CConfig *config) |
| Load the geometries at the previous time states n and nM1. More... | |
| virtual void | Postprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, CNumerics **numerics, unsigned short iMesh) |
| A virtual member, overloaded. More... | |
| virtual void | Preprocessing (CGeometry *geometry, CSolver **solver_container, CConfig *config, CNumerics **numerics, unsigned short iMesh, unsigned long Iteration, unsigned short RunTime_EqSystem, bool Output) |
| A virtual member overloaded. More... | |
| virtual void | BC_Clamped (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Clamped_Post (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Normal_Displacement (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Normal_Load (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Dir_Load (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Sine_Load (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Pressure (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Neumann (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Dielec (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | BC_Electrode (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config, unsigned short val_marker) |
| A virtual member. More... | |
| virtual void | ImplicitNewmark_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | ImplicitNewmark_Update (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | ImplicitNewmark_Relaxation (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | GeneralizedAlpha_Iteration (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | GeneralizedAlpha_UpdateDisp (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | GeneralizedAlpha_UpdateSolution (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | GeneralizedAlpha_UpdateLoads (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | Compute_Residual (CGeometry *geometry, CSolver **solver_container, CConfig *config, unsigned short iMesh) |
| A virtual member. More... | |
| virtual void | Inviscid_DeltaForces (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | Viscous_DeltaForces (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | Wave_Strength (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | SetPrimitive_Limiter_MPI (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | AddStiffMatrix (su2double **StiffMatrix_Elem, unsigned long Point_0, unsigned long Point_1, unsigned long Point_2, unsigned long Point_3) |
| A virtual member. More... | |
| virtual void | SetCSensitivity (unsigned short val_marker, unsigned long val_vertex, su2double val_sensitivity) |
| A virtual member. More... | |
| virtual void | SetForceProj_Vector (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | SetIntBoundary_Jump (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | SetDistance (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | Inviscid_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config) |
| A virtual member. More... | |
| virtual void | Smooth_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config) |
| A virtual member. More... | |
| virtual void | Viscous_Sensitivity (CGeometry *geometry, CSolver **solver_container, CNumerics *numerics, CConfig *config) |
| A virtual member. More... | |
| virtual su2double | Get_PressureDrag (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| virtual su2double | Get_ViscDrag (void) |
| Provide the total (inviscid + viscous) non dimensional drag coefficient. More... | |
| virtual su2double | GetTotal_CFEA (void) |
| A virtual member. More... | |
| virtual void | SetTotal_CFEA (su2double val_cfea) |
| A virtual member. More... | |
| virtual su2double | GetTotal_CWave (void) |
| A virtual member. More... | |
| virtual su2double | GetTotal_CHeat (void) |
| A virtual member. More... | |
| virtual void | SetDonorAdjVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var, su2double val_value) |
| A virtual member. More... | |
| virtual su2double * | GetDonorAdjVar (unsigned short val_marker, unsigned long val_vertex) |
| A virtual member. More... | |
| virtual su2double | GetDonorAdjVar (unsigned short val_marker, unsigned long val_vertex, unsigned short val_var) |
| A virtual member. More... | |
| virtual su2double | GetPsiRho_Inf (void) |
| A virtual member. More... | |
| virtual su2double * | GetPsiRhos_Inf (void) |
| A virtual member. More... | |
| virtual su2double | GetPsiE_Inf (void) |
| A virtual member. More... | |
| virtual su2double | GetPhi_Inf (unsigned short val_dim) |
| A virtual member. More... | |
| virtual su2double | GetTotal_Sens_Geo (void) |
| A virtual member. More... | |
| virtual su2double | GetTotal_Sens_Mach (void) |
| A virtual member. More... | |
| virtual su2double | GetTotal_Sens_AoA (void) |
| A virtual member. More... | |
| virtual su2double | GetTotal_Sens_Press (void) |
| Set the total farfield pressure sensitivity coefficient. More... | |
| virtual su2double | GetTotal_Sens_Temp (void) |
| Set the total farfield temperature sensitivity coefficient. More... | |
| virtual su2double | GetTotal_Sens_BPress (void) |
| Get the total back pressure sensitivity coefficient. More... | |
| virtual su2double | GetDensity_Inf (unsigned short val_var) |
| A virtual member. More... | |
| virtual su2double | GetDensity_Velocity_Inf (unsigned short val_dim, unsigned short val_var) |
| A virtual member. More... | |
| virtual su2double | GetCSensitivity (unsigned short val_marker, unsigned long val_vertex) |
| A virtual member. More... | |
| virtual su2double * | GetConstants () |
| A virtual member. More... | |
| virtual void | SetFEA_Load (CSolver ***flow_solution, CGeometry **fea_geometry, CGeometry **flow_geometry, CConfig *fea_config, CConfig *flow_config, CNumerics *fea_numerics) |
| A virtual member. More... | |
| virtual void | SetFEA_Load_Int (CSolver ***flow_solution, CGeometry **fea_geometry, CGeometry **flow_geometry, CConfig *fea_config, CConfig *flow_config, CNumerics *fea_numerics) |
| A virtual member. More... | |
| virtual void | Copy_Zone_Solution (CSolver ***solver1_solution, CGeometry **solver1_geometry, CConfig *solver1_config, CSolver ***solver2_solution, CGeometry **solver2_geometry, CConfig *solver2_config) |
| A virtual member. More... | |
| virtual void | ResetInitialCondition (CGeometry **geometry, CSolver ***solver_container, CConfig *config, unsigned long ExtIter) |
| A virtual member. More... | |
| virtual void | PredictStruct_Displacement (CGeometry **fea_geometry, CConfig *fea_config, CSolver ***fea_solution) |
| A virtual member. More... | |
| virtual void | ComputeAitken_Coefficient (CGeometry **fea_geometry, CConfig *fea_config, CSolver ***fea_solution, unsigned long iFSIIter) |
| A virtual member. More... | |
| virtual void | SetAitken_Relaxation (CGeometry **fea_geometry, CConfig *fea_config, CSolver ***fea_solution) |
| A virtual member. More... | |
| virtual void | Update_StructSolution (CGeometry **fea_geometry, CConfig *fea_config, CSolver ***fea_solution) |
| A virtual member. More... | |
| virtual void | LoadRestart_FSI (CGeometry *geometry, CSolver ***solver, CConfig *config, int val_iter) |
| A virtual member. More... | |
| void | Gauss_Elimination (su2double **A, su2double *rhs, unsigned short nVar) |
| Gauss method for solving a linear system. More... | |
| void | Aeroelastic (CSurfaceMovement *surface_movement, CGeometry *geometry, CConfig *config, unsigned long ExtIter) |
| Prepares and solves the aeroelastic equations. More... | |
| void | SetUpTypicalSectionWingModel (vector< vector< su2double > > &PHI, vector< su2double > &w, CConfig *config) |
| Sets up the generalized eigenvectors and eigenvalues needed to solve the aeroelastic equations. More... | |
| void | SolveTypicalSectionWingModel (CGeometry *geometry, su2double Cl, su2double Cm, CConfig *config, unsigned short val_Marker, vector< su2double > &displacements) |
| Solve the typical section wing model. More... | |
| virtual void | RegisterSolution (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | RegisterOutput (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | SetAdjoint_Output (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | ExtractAdjoint_Solution (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | RegisterObj_Func (CConfig *config) |
| A virtual member. More... | |
| virtual void | SetSurface_Sensitivity (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | SetSensitivity (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | SetAdj_ObjFunc (CGeometry *geometry, CConfig *config) |
| virtual void | SetFSI_ConvValue (unsigned short val_index, su2double val_criteria) |
| A virtual member. More... | |
| virtual su2double | GetFSI_ConvValue (unsigned short val_index) |
| A virtual member. More... | |
| virtual void | Set_Prestretch (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
| virtual void | Compute_StiffMatrix (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config) |
| A virtual member. More... | |
| virtual void | Compute_StiffMatrix_NodalStressRes (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config) |
| A virtual member. More... | |
| virtual void | Compute_MassMatrix (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config) |
| A virtual member. More... | |
| virtual void | Compute_NodalStressRes (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config) |
| A virtual member. More... | |
| virtual void | Compute_NodalStress (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config) |
| A virtual member. More... | |
| virtual void | Compute_DeadLoad (CGeometry *geometry, CSolver **solver_container, CNumerics **numerics, CConfig *config) |
| A virtual member. More... | |
| virtual void | Solve_System (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | Initialize_SystemMatrix (CGeometry *geometry, CSolver **solver_container, CConfig *config) |
| A virtual member. More... | |
| virtual void | Compute_IntegrationConstants (CConfig *config) |
| A virtual member. More... | |
| virtual su2double | GetWAitken_Dyn (void) |
| A virtual member. More... | |
| virtual su2double | GetWAitken_Dyn_tn1 (void) |
| A virtual member. More... | |
| virtual void | SetWAitken_Dyn (su2double waitk) |
| A virtual member. More... | |
| virtual void | SetWAitken_Dyn_tn1 (su2double waitk_tn1) |
| A virtual member. More... | |
| virtual void | SetLoad_Increment (su2double val_loadIncrement) |
| A virtual member. More... | |
| virtual void | SetRecording (CGeometry *geometry, CConfig *config, unsigned short kind_recording) |
| A virtual member. More... | |
| virtual void | RegisterVariables (CGeometry *geometry, CConfig *config, bool reset=false) |
| A virtual member. More... | |
| virtual void | ExtractAdjoint_Variables (CGeometry *geometry, CConfig *config) |
| A virtual member. More... | |
Additional Inherited Members | |
| Static Public Member Functions inherited from CEulerSolver | |
| static bool | Compareval (std::vector< su2double > a, std::vector< su2double > b) |
| compare to values. More... | |
| Public Attributes inherited from CSolver | |
| CSysVector | LinSysSol |
| vector to store iterative solution of implicit linear system. | |
| CSysVector | LinSysRes |
| vector to store iterative residual of implicit linear system. | |
| CSysVector | LinSysAux |
| vector to store iterative residual of implicit linear system. | |
| CSysMatrix | Jacobian |
| Complete sparse Jacobian structure for implicit computations. | |
| CSysMatrix | StiffMatrix |
| Sparse structure for storing the stiffness matrix in Galerkin computations, and grid movement. | |
| CSysVector | OutputVariables |
| vector to store the extra variables to be written. | |
| string * | OutputHeadingNames |
| CVariable ** | node |
| Vector which the define the variables for each problem. | |
| CVariable * | node_infty |
| CVariable storing the free stream conditions. | |
| Protected Attributes inherited from CEulerSolver | |
| su2double | Mach_Inf |
| Mach number at the infinity. | |
| su2double | Density_Inf |
| Density at the infinity. | |
| su2double | Energy_Inf |
| Energy at the infinity. | |
| su2double | Temperature_Inf |
| Energy at the infinity. | |
| su2double | Pressure_Inf |
| Pressure at the infinity. | |
| su2double * | Velocity_Inf |
| Flow Velocity vector at the infinity. | |
| su2double * | CD_Inv |
| Drag coefficient (inviscid contribution) for each boundary. | |
| su2double * | CL_Inv |
| Lift coefficient (inviscid contribution) for each boundary. | |
| su2double * | CSF_Inv |
| Sideforce coefficient (inviscid contribution) for each boundary. | |
| su2double * | CMx_Inv |
| x Moment coefficient (inviscid contribution) for each boundary. | |
| su2double * | CMy_Inv |
| y Moment coefficient (inviscid contribution) for each boundary. | |
| su2double * | CMz_Inv |
| z Moment coefficient (inviscid contribution) for each boundary. | |
| su2double * | CFx_Inv |
| x Force coefficient (inviscid contribution) for each boundary. | |
| su2double * | CFy_Inv |
| y Force coefficient (inviscid contribution) for each boundary. | |
| su2double * | CFz_Inv |
| z Force coefficient (inviscid contribution) for each boundary. | |
| su2double * | Surface_CL_Inv |
| Lift coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CD_Inv |
| Drag coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CSF_Inv |
| Side-force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CEff_Inv |
| Side-force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CFx_Inv |
| x Force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CFy_Inv |
| y Force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CFz_Inv |
| z Force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CMx_Inv |
| x Moment coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CMy_Inv |
| y Moment coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CMz_Inv |
| z Moment coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | CEff_Inv |
| Efficiency (Cl/Cd) (inviscid contribution) for each boundary. | |
| su2double * | CMerit_Inv |
| Rotor Figure of Merit (inviscid contribution) for each boundary. | |
| su2double * | CT_Inv |
| Thrust coefficient (force in -x direction, inviscid contribution) for each boundary. | |
| su2double * | CQ_Inv |
| Torque coefficient (moment in -x direction, inviscid contribution) for each boundary. | |
| su2double * | CEquivArea_Inv |
| Equivalent area (inviscid contribution) for each boundary. | |
| su2double * | CNearFieldOF_Inv |
| Near field pressure (inviscid contribution) for each boundary. | |
| su2double * | CD_Mnt |
| Drag coefficient (inviscid contribution) for each boundary. | |
| su2double * | CL_Mnt |
| Lift coefficient (inviscid contribution) for each boundary. | |
| su2double * | CSF_Mnt |
| Sideforce coefficient (inviscid contribution) for each boundary. | |
| su2double * | CMx_Mnt |
| x Moment coefficient (inviscid contribution) for each boundary. | |
| su2double * | CMy_Mnt |
| y Moment coefficient (inviscid contribution) for each boundary. | |
| su2double * | CMz_Mnt |
| z Moment coefficient (inviscid contribution) for each boundary. | |
| su2double * | CFx_Mnt |
| x Force coefficient (inviscid contribution) for each boundary. | |
| su2double * | CFy_Mnt |
| y Force coefficient (inviscid contribution) for each boundary. | |
| su2double * | CFz_Mnt |
| z Force coefficient (inviscid contribution) for each boundary. | |
| su2double * | Surface_CL_Mnt |
| Lift coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CD_Mnt |
| Drag coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CSF_Mnt |
| Side-force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CEff_Mnt |
| Side-force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CFx_Mnt |
| x Force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CFy_Mnt |
| y Force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CFz_Mnt |
| z Force coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CMx_Mnt |
| x Moment coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CMy_Mnt |
| y Moment coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | Surface_CMz_Mnt |
| z Moment coefficient (inviscid contribution) for each monitoring surface. | |
| su2double * | CEff_Mnt |
| Efficiency (Cl/Cd) (inviscid contribution) for each boundary. | |
| su2double * | CMerit_Mnt |
| Rotor Figure of Merit (inviscid contribution) for each boundary. | |
| su2double * | CT_Mnt |
| Thrust coefficient (force in -x direction, inviscid contribution) for each boundary. | |
| su2double * | CQ_Mnt |
| Torque coefficient (moment in -x direction, inviscid contribution) for each boundary. | |
| su2double * | CEquivArea_Mnt |
| Equivalent area (inviscid contribution) for each boundary. | |
| su2double ** | CPressure |
| Pressure coefficient for each boundary and vertex. | |
| su2double ** | CPressureTarget |
| Target Pressure coefficient for each boundary and vertex. | |
| su2double ** | HeatFlux |
| Heat transfer coefficient for each boundary and vertex. | |
| su2double ** | HeatFluxTarget |
| Heat transfer coefficient for each boundary and vertex. | |
| su2double ** | YPlus |
| Yplus for each boundary and vertex. | |
| su2double *** | CharacPrimVar |
| Value of the characteristic variables at each boundary. | |
| su2double *** | DonorPrimVar |
| Value of the donor variables at each boundary. | |
| su2double * | ForceInviscid |
| Inviscid force for each boundary. | |
| su2double * | MomentInviscid |
| Inviscid moment for each boundary. | |
| su2double * | ForceMomentum |
| Inviscid force for each boundary. | |
| su2double * | MomentMomentum |
| Inviscid moment for each boundary. | |
| su2double * | Inflow_MassFlow |
| Mass flow rate for each boundary. | |
| su2double * | Exhaust_MassFlow |
| Mass flow rate for each boundary. | |
| su2double * | Inflow_Pressure |
| Fan face pressure for each boundary. | |
| su2double * | Inflow_Mach |
| Fan face mach number for each boundary. | |
| su2double * | Inflow_Area |
| Boundary total area. | |
| su2double * | Exhaust_Area |
| Boundary total area. | |
| su2double * | Exhaust_Pressure |
| Fan face pressure for each boundary. | |
| su2double * | Exhaust_Temperature |
| Fan face mach number for each boundary. | |
| su2double | Inflow_MassFlow_Total |
| Mass flow rate for each boundary. | |
| su2double | Exhaust_MassFlow_Total |
| Mass flow rate for each boundary. | |
| su2double | Inflow_Pressure_Total |
| Fan face pressure for each boundary. | |
| su2double | Inflow_Mach_Total |
| Fan face mach number for each boundary. | |
| su2double | InverseDesign |
| Inverse design functional for each boundary. | |
| unsigned long ** | DonorGlobalIndex |
| Value of the donor global index. | |
| su2double ** | ActDisk_DeltaP |
| Value of the Delta P. | |
| su2double ** | ActDisk_DeltaT |
| Value of the Delta T. | |
| su2double ** | Inlet_Ptotal |
| Value of the Total P. | |
| su2double ** | Inlet_Ttotal |
| Value of the Total T. | |
| su2double *** | Inlet_FlowDir |
| Value of the Flow Direction. | |
| su2double | AllBound_CD_Inv |
| Total drag coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CL_Inv |
| Total lift coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CSF_Inv |
| Total sideforce coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CMx_Inv |
| Total x moment coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CMy_Inv |
| Total y moment coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CMz_Inv |
| Total z moment coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CFx_Inv |
| Total x force coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CFy_Inv |
| Total y force coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CFz_Inv |
| Total z force coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CEff_Inv |
| Efficient coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CMerit_Inv |
| Rotor Figure of Merit (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CT_Inv |
| Total thrust coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CQ_Inv |
| Total torque coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CEquivArea_Inv |
| equivalent area coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CNearFieldOF_Inv |
| Near-Field press coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CD_Mnt |
| Total drag coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CL_Mnt |
| Total lift coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CSF_Mnt |
| Total sideforce coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CMx_Mnt |
| Total x moment coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CMy_Mnt |
| Total y moment coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CMz_Mnt |
| Total z moment coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CFx_Mnt |
| Total x force coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CFy_Mnt |
| Total y force coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CFz_Mnt |
| Total z force coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CEff_Mnt |
| Efficient coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CMerit_Mnt |
| Rotor Figure of Merit (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CT_Mnt |
| Total thrust coefficient (inviscid contribution) for all the boundaries. | |
| su2double | AllBound_CQ_Mnt |
| Total torque coefficient (inviscid contribution) for all the boundaries. | |
| su2double | OneD_TotalPress |
| average total pressure evaluated at an exit | |
| su2double | OneD_Mach |
| area average Mach evaluated at an exit | |
| su2double | OneD_Temp |
| area average Temperature evaluated at an exit | |
| su2double | OneD_PressureRef |
| area average Pressure evaluated at an exit | |
| su2double | OneD_MassFlowRate |
| Mass flow rate at an exit. | |
| su2double | OneD_DensityRef |
| flux average density evaluated at an exit | |
| su2double | OneD_EnthalpyRef |
| flux average enthalpy evaluated at an exit | |
| su2double | OneD_VelocityRef |
| flux average velocity evaluated at an exit | |
| su2double | Total_ComboObj |
| Total 'combo' objective for all monitored boundaries. | |
| su2double | AoA_Prev |
| Old value of the AoA for fixed lift mode. | |
| su2double | Total_CD |
| Total drag coefficient for all the boundaries. | |
| su2double | Total_CL |
| Total lift coefficient for all the boundaries. | |
| su2double | Total_CL_Prev |
| Total lift coefficient for all the boundaries (fixed lift mode). | |
| su2double | Total_CD_SolidSurf |
| Total drag coefficient for all the boundaries. | |
| su2double | Total_CD_Prev |
| Total drag coefficient for all the boundaries (fixed lift mode). | |
| su2double | Total_NetCThrust |
| Total drag coefficient for all the boundaries. | |
| su2double | Total_Power |
| Total drag coefficient for all the boundaries. | |
| su2double | Total_ReverseFlow |
| Total drag coefficient for all the boundaries. | |
| su2double | Total_IDC |
| Total IDC coefficient for all the boundaries. | |
| su2double | Total_IDC_Mach |
| Total IDC coefficient for all the boundaries. | |
| su2double | Total_IDR |
| Total IDC coefficient for all the boundaries. | |
| su2double | Total_DC60 |
| Total IDC coefficient for all the boundaries. | |
| su2double | Total_MFR |
| Total Mass Flow Ratio for all the boundaries. | |
| su2double | Total_Prop_Eff |
| Total Mass Flow Ratio for all the boundaries. | |
| su2double | Total_ByPassProp_Eff |
| Total Mass Flow Ratio for all the boundaries. | |
| su2double | Total_Adiab_Eff |
| Total Mass Flow Ratio for all the boundaries. | |
| su2double | Total_Poly_Eff |
| Total Mass Flow Ratio for all the boundaries. | |
| su2double | Total_NetCThrust_Prev |
| Total lift coefficient for all the boundaries. | |
| su2double | Total_BCThrust_Prev |
| Total lift coefficient for all the boundaries. | |
| su2double | Total_Custom |
| Total IDC coefficient for all the boundaries. | |
| su2double | Total_CSF |
| Total sideforce coefficient for all the boundaries. | |
| su2double | Total_CMx |
| Total x moment coefficient for all the boundaries. | |
| su2double | Total_CMy |
| Total y moment coefficient for all the boundaries. | |
| su2double | Total_CMz |
| Total z moment coefficient for all the boundaries. | |
| su2double | Total_CFx |
| Total x force coefficient for all the boundaries. | |
| su2double | Total_CFy |
| Total y force coefficient for all the boundaries. | |
| su2double | Total_CFz |
| Total z force coefficient for all the boundaries. | |
| su2double | Total_CEff |
| Total efficiency coefficient for all the boundaries. | |
| su2double | Total_CMerit |
| Total rotor Figure of Merit for all the boundaries. | |
| su2double | Total_CT |
| Total thrust coefficient for all the boundaries. | |
| su2double | Total_CQ |
| Total torque coefficient for all the boundaries. | |
| su2double | Total_Heat |
| Total heat load for all the boundaries. | |
| su2double | Total_MaxHeat |
| Maximum heat flux on all boundaries. | |
| su2double | Total_AeroCD |
| Total aero drag coefficient for all the boundaries. | |
| su2double | Total_RadialDistortion |
| Total fan face radial distortion for all the boundaries. | |
| su2double | Total_CircumferentialDistortion |
| Total fan face circumferential distortion for all the boundaries. | |
| su2double | Total_CEquivArea |
| Total Equivalent Area coefficient for all the boundaries. | |
| su2double | Total_CNearFieldOF |
| Total Near-Field Pressure coefficient for all the boundaries. | |
| su2double | Total_CpDiff |
| Total Equivalent Area coefficient for all the boundaries. | |
| su2double | Total_HeatFluxDiff |
| Total Equivalent Area coefficient for all the boundaries. | |
| su2double | Total_MassFlowRate |
| Total Mass Flow Rate on monitored boundaries. | |
| su2double * | Surface_CL |
| Lift coefficient for each monitoring surface. | |
| su2double * | Surface_CD |
| Drag coefficient for each monitoring surface. | |
| su2double * | Surface_CSF |
| Side-force coefficient for each monitoring surface. | |
| su2double * | Surface_CEff |
| Side-force coefficient for each monitoring surface. | |
| su2double * | Surface_CFx |
| x Force coefficient for each monitoring surface. | |
| su2double * | Surface_CFy |
| y Force coefficient for each monitoring surface. | |
| su2double * | Surface_CFz |
| z Force coefficient for each monitoring surface. | |
| su2double * | Surface_CMx |
| x Moment coefficient for each monitoring surface. | |
| su2double * | Surface_CMy |
| y Moment coefficient for each monitoring surface. | |
| su2double * | Surface_CMz |
| z Moment coefficient for each monitoring surface. | |
| su2double * | Surface_HF_Visc |
| Total (integrated) heat flux for each monitored surface. | |
| su2double * | Surface_MaxHF_Visc |
| Maximum heat flux for each monitored surface. | |
| su2double * | iPoint_UndLapl |
| Auxiliary variable for the undivided Laplacians. | |
| su2double * | jPoint_UndLapl |
| Auxiliary variable for the undivided Laplacians. | |
| su2double * | SecondaryVar_i |
| Auxiliary vector for storing the solution at point i. | |
| su2double * | SecondaryVar_j |
| Auxiliary vector for storing the solution at point j. | |
| su2double * | PrimVar_i |
| Auxiliary vector for storing the solution at point i. | |
| su2double * | PrimVar_j |
| Auxiliary vector for storing the solution at point j. | |
| su2double ** | LowMach_Precontioner |
| Auxiliary vector for storing the inverse of Roe-turkel preconditioner. | |
| unsigned long | nMarker |
| Total number of markers using the grid information. | |
| unsigned long * | nVertex |
| Store nVertex at each marker for deallocation. | |
| bool | space_centered |
| True if space centered scheeme used. | |
| bool | euler_implicit |
| True if euler implicit scheme used. | |
| bool | least_squares |
| True if computing gradients by least squares. | |
| su2double | Gamma |
| Fluid's Gamma constant (ratio of specific heats). | |
| su2double | Gamma_Minus_One |
| Fluids's Gamma - 1.0 . | |
| su2double * | Primitive |
| Auxiliary nPrimVar vector. | |
| su2double * | Primitive_i |
| Auxiliary nPrimVar vector for storing the primitive at point i. | |
| su2double * | Primitive_j |
| Auxiliary nPrimVar vector for storing the primitive at point j. | |
| su2double * | Secondary |
| Auxiliary nPrimVar vector. | |
| su2double * | Secondary_i |
| Auxiliary nPrimVar vector for storing the primitive at point i. | |
| su2double * | Secondary_j |
| Auxiliary nPrimVar vector for storing the primitive at point j. | |
| su2double | Cauchy_Value |
| Summed value of the convergence indicator. | |
| su2double | Cauchy_Func |
| Current value of the convergence indicator at one iteration. | |
| unsigned short | Cauchy_Counter |
| Number of elements of the Cauchy serial. | |
| su2double * | Cauchy_Serie |
| Complete Cauchy serial. | |
| su2double | Old_Func |
| Old value of the objective function (the function which is monitored). | |
| su2double | New_Func |
| Current value of the objective function (the function which is monitored). | |
| su2double | AoA_old |
| Old value of the angle of attack (monitored). | |
| unsigned long | AoA_Counter |
| unsigned long | BCThrust_Counter |
| CFluidModel * | FluidModel |
| fluid model used in the solver | |
| su2double ** | AveragedVelocity |
| su2double ** | AveragedNormal |
| su2double ** | AveragedGridVel |
| su2double ** | AveragedFlux |
| su2double ** | TotalFlux |
| su2double * | TotalArea |
| su2double * | AveragedNormalVelocity |
| su2double * | ExtAveragedNormalVelocity |
| su2double * | AveragedTangVelocity |
| su2double * | ExtAveragedTangVelocity |
| su2double * | AveragedTangGridVelocity |
| su2double * | AveragedMach |
| su2double * | AveragedNormalMach |
| su2double * | AveragedTangMach |
| su2double * | AveragedEnthalpy |
| su2double * | AveragedPressure |
| su2double * | AveragedTotTemperature |
| su2double * | AveragedTotPressure |
| su2double * | ExtAveragedPressure |
| su2double * | ExtAveragedTotTemperature |
| su2double * | ExtAveragedTotPressure |
| su2double * | AveragedDensity |
| su2double * | ExtAveragedDensity |
| su2double * | AveragedSoundSpeed |
| su2double * | AveragedEntropy |
| su2double * | MassFlow |
| su2double * | FlowAngle |
| su2double * | TotalStaticEfficiency |
| su2double * | TotalTotalEfficiency |
| su2double * | KineticEnergyLoss |
| su2double * | TotalPressureLoss |
| su2double * | MassFlowIn |
| su2double * | MassFlowOut |
| su2double * | FlowAngleIn |
| su2double * | FlowAngleOut |
| su2double * | EulerianWork |
| su2double * | TotalEnthalpyIn |
| su2double * | PressureRatio |
| su2double * | PressureOut |
| su2double * | EnthalpyOut |
| su2double * | MachIn |
| su2double * | MachOut |
| su2double * | NormalMachIn |
| su2double * | NormalMachOut |
| su2double * | VelocityOutIs |
| su2double *** | SlidingState |
| Protected Attributes inherited from CSolver | |
| unsigned short | IterLinSolver |
| Linear solver iterations. | |
| unsigned short | nVar |
| Number of variables of the problem. | |
| unsigned short | nPrimVar |
| Number of primitive variables of the problem. | |
| unsigned short | nPrimVarGrad |
| Number of primitive variables of the problem in the gradient computation. | |
| unsigned short | nSecondaryVar |
| Number of primitive variables of the problem. | |
| unsigned short | nSecondaryVarGrad |
| Number of primitive variables of the problem in the gradient computation. | |
| unsigned short | nVarGrad |
| Number of variables for deallocating the LS Cvector. | |
| unsigned short | nDim |
| Number of dimensions of the problem. | |
| unsigned long | nPoint |
| Number of points of the computational grid. | |
| unsigned long | nPointDomain |
| Number of points of the computational grid. | |
| su2double | Max_Delta_Time |
| Maximum value of the delta time for all the control volumes. | |
| su2double | Min_Delta_Time |
| Minimum value of the delta time for all the control volumes. | |
| su2double * | Residual_RMS |
| Vector with the mean residual for each variable. | |
| su2double * | Residual_Max |
| Vector with the maximal residual for each variable. | |
| su2double * | Residual |
| Auxiliary nVar vector. | |
| su2double * | Residual_i |
| Auxiliary nVar vector for storing the residual at point i. | |
| su2double * | Residual_j |
| Auxiliary nVar vector for storing the residual at point j. | |
| unsigned long * | Point_Max |
| Vector with the maximal residual for each variable. | |
| su2double ** | Point_Max_Coord |
| Vector with pointers to the coords of the maximal residual for each variable. | |
| su2double * | Solution |
| Auxiliary nVar vector. | |
| su2double * | Solution_i |
| Auxiliary nVar vector for storing the solution at point i. | |
| su2double * | Solution_j |
| Auxiliary nVar vector for storing the solution at point j. | |
| su2double * | Vector |
| Auxiliary nDim vector. | |
| su2double * | Vector_i |
| Auxiliary nDim vector to do the reconstruction of the variables at point i. | |
| su2double * | Vector_j |
| Auxiliary nDim vector to do the reconstruction of the variables at point j. | |
| su2double * | Res_Conv |
| Auxiliary nVar vector for storing the convective residual. | |
| su2double * | Res_Visc |
| Auxiliary nVar vector for storing the viscous residual. | |
| su2double * | Res_Sour |
| Auxiliary nVar vector for storing the viscous residual. | |
| su2double * | Res_Conv_i |
| Auxiliary vector for storing the convective residual at point i. | |
| su2double * | Res_Visc_i |
| Auxiliary vector for storing the viscous residual at point i. | |
| su2double * | Res_Conv_j |
| Auxiliary vector for storing the convective residual at point j. | |
| su2double * | Res_Visc_j |
| Auxiliary vector for storing the viscous residual at point j. | |
| su2double ** | Jacobian_i |
| Auxiliary matrices for storing point to point Jacobians at point i. | |
| su2double ** | Jacobian_j |
| Auxiliary matrices for storing point to point Jacobians at point j. | |
| su2double ** | Jacobian_ii |
| Auxiliary matrices for storing point to point Jacobians. | |
| su2double ** | Jacobian_ij |
| Auxiliary matrices for storing point to point Jacobians. | |
| su2double ** | Jacobian_ji |
| Auxiliary matrices for storing point to point Jacobians. | |
| su2double ** | Jacobian_jj |
| Auxiliary matrices for storing point to point Jacobians. | |
| su2double ** | Smatrix |
| Auxiliary structure for computing gradients by least-squares. | |
| su2double ** | Cvector |
| Auxiliary structure for computing gradients by least-squares. | |
| unsigned short | nOutputVariables |
| Number of variables to write. | |
Detailed Description
Main class for defining the Navier-Stokes flow solver.
- Version
- 5.0.0 "Raven"
Constructor & Destructor Documentation
§ CNSSolver()
This is an overloaded member function, provided for convenience. It differs from the above function only in what argument(s) it accepts.
- Parameters
-
[in] geometry - Geometrical definition of the problem. [in] config - Definition of the particular problem.
Member Function Documentation
§ BC_HeatFlux_Wall()
|
virtual |
Impose a constant heat-flux condition at the wall.
- Parameters
-
[in] geometry - Geometrical definition of the problem. [in] solver_container - Container vector with all the solutions. [in] conv_numerics - Description of the numerical method. [in] visc_numerics - Description of the numerical method. [in] config - Definition of the particular problem. [in] val_marker - Surface marker where the boundary condition is applied.
Reimplemented from CSolver.
§ BC_Isothermal_Wall()
|
virtual |
Impose the Navier-Stokes boundary condition (strong).
- Parameters
-
[in] geometry - Geometrical definition of the problem. [in] solver_container - Container vector with all the solutions. [in] conv_numerics - Description of the numerical method. [in] visc_numerics - Description of the numerical method. [in] config - Definition of the particular problem. [in] val_marker - Surface marker where the boundary condition is applied.
Reimplemented from CSolver.
§ Friction_Forces()
Compute the viscous forces and all the addimensional coefficients.
- Parameters
-
[in] geometry - Geometrical definition of the problem. [in] config - Definition of the particular problem.
Reimplemented from CSolver.
§ GetAllBound_CD_Visc()
|
inlinevirtual |
Get the inviscid contribution to the drag coefficient.
- Returns
- Value of the drag coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CEff_Visc()
|
inlinevirtual |
Get the inviscid contribution to the efficiency coefficient.
- Returns
- Value of the efficiency coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CFx_Visc()
|
inlinevirtual |
Get the inviscid contribution to the efficiency coefficient.
- Returns
- Value of the efficiency coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CFy_Visc()
|
inlinevirtual |
Get the inviscid contribution to the efficiency coefficient.
- Returns
- Value of the efficiency coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CFz_Visc()
|
inlinevirtual |
Get the inviscid contribution to the efficiency coefficient.
- Returns
- Value of the efficiency coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CL_Visc()
|
inlinevirtual |
Get the inviscid contribution to the lift coefficient.
- Returns
- Value of the lift coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CMx_Visc()
|
inlinevirtual |
Get the inviscid contribution to the efficiency coefficient.
- Returns
- Value of the efficiency coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CMy_Visc()
|
inlinevirtual |
Get the inviscid contribution to the efficiency coefficient.
- Returns
- Value of the efficiency coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CMz_Visc()
|
inlinevirtual |
Get the inviscid contribution to the efficiency coefficient.
- Returns
- Value of the efficiency coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetAllBound_CSF_Visc()
|
inlinevirtual |
Get the inviscid contribution to the sideforce coefficient.
- Returns
- Value of the sideforce coefficient (inviscid contribution).
Reimplemented from CSolver.
§ GetCD_Visc()
|
inlinevirtual |
Get the non dimensional drag coefficient (viscous contribution).
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the drag coefficient (viscous contribution) on the surface val_marker.
Reimplemented from CSolver.
§ GetCL_Visc()
|
inlinevirtual |
Get the non dimensional lift coefficient (viscous contribution).
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the lift coefficient (viscous contribution) on the surface val_marker.
Reimplemented from CSolver.
§ GetCMz_Visc()
|
inlinevirtual |
Get the non dimensional z moment coefficient (viscous contribution).
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the z moment coefficient (viscous contribution) on the surface val_marker.
Reimplemented from CSolver.
§ GetCSF_Visc()
|
inlinevirtual |
Get the non dimensional sideforce coefficient (viscous contribution).
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the sideforce coefficient (viscous contribution) on the surface val_marker.
Reimplemented from CSolver.
§ GetCSkinFriction()
|
inlinevirtual |
Get the skin friction coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed. [in] val_vertex - Vertex of the marker val_marker where the coefficient is evaluated.
- Returns
- Value of the skin friction coefficient.
Reimplemented from CSolver.
§ GetHeatFlux()
|
inlinevirtual |
Get the skin friction coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed. [in] val_vertex - Vertex of the marker val_marker where the coefficient is evaluated.
- Returns
- Value of the heat transfer coefficient.
Reimplemented from CSolver.
§ GetHeatFluxTarget()
|
inlinevirtual |
Get the skin friction coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed. [in] val_vertex - Vertex of the marker val_marker where the coefficient is evaluated.
- Returns
- Value of the heat transfer coefficient.
Reimplemented from CSolver.
§ GetOmega_Max()
|
inlinevirtual |
§ GetStrainMag_Max()
|
inlinevirtual |
Get the max Strain rate magnitude.
- Returns
- Value of the max Strain rate magnitude.
Reimplemented from CSolver.
§ GetSurface_CD_Visc()
|
inlinevirtual |
Provide the non dimensional drag coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the drag coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CEff_Visc()
|
inlinevirtual |
Provide the non dimensional side-force coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the side-force coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CFx_Visc()
|
inlinevirtual |
Provide the non dimensional x force coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the x force coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CFy_Visc()
|
inlinevirtual |
Provide the non dimensional y force coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the y force coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CFz_Visc()
|
inlinevirtual |
Provide the non dimensional z force coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the z force coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CL_Visc()
|
inlinevirtual |
Provide the non dimensional lift coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the lift coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CMx_Visc()
|
inlinevirtual |
Provide the non dimensional x moment coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the x moment coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CMy_Visc()
|
inlinevirtual |
Provide the non dimensional y moment coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the y moment coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CMz_Visc()
|
inlinevirtual |
Provide the non dimensional z moment coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the z moment coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_CSF_Visc()
|
inlinevirtual |
Provide the non dimensional side-force coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed.
- Returns
- Value of the side-force coefficient on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_HF_Visc()
|
inlinevirtual |
Get the total heat flux.
- Parameters
-
[in] val_marker - Surface marker where the heat flux is computed.
- Returns
- Value of the integrated heat flux (viscous contribution) on the surface val_marker.
Reimplemented from CSolver.
§ GetSurface_MaxHF_Visc()
|
inlinevirtual |
Get the maximum (per surface) heat flux.
- Parameters
-
[in] val_marker - Surface marker where the heat flux is computed.
- Returns
- Value of the maximum heat flux (viscous contribution) on the surface val_marker.
Reimplemented from CSolver.
§ GetTke_Inf()
|
inlinevirtual |
Get the turbulent kinetic energy at the infinity.
- Returns
- Value of the turbulent kinetic energy at the infinity.
Reimplemented from CSolver.
§ GetViscosity_Inf()
|
inlinevirtual |
Compute the viscosity at the infinity.
- Returns
- Value of the viscosity at the infinity.
Reimplemented from CSolver.
§ GetYPlus()
|
inlinevirtual |
Get the y plus.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed. [in] val_vertex - Vertex of the marker val_marker where the coefficient is evaluated.
- Returns
- Value of the y plus.
Reimplemented from CSolver.
§ Preprocessing()
|
virtual |
Restart residual and compute gradients.
- Parameters
-
[in] geometry - Geometrical definition of the problem. [in] solver_container - Container vector with all the solutions. [in] config - Definition of the particular problem. [in] iRKStep - Current step of the Runge-Kutta iteration. [in] RunTime_EqSystem - System of equations which is going to be solved. [in] Output - boolean to determine whether to print output.
Reimplemented from CEulerSolver.
§ SetHeatFluxTarget()
|
inlinevirtual |
Set the value of the target Pressure coefficient.
- Parameters
-
[in] val_marker - Surface marker where the coefficient is computed. [in] val_vertex - Vertex of the marker val_marker where the coefficient is evaluated.
- Returns
- Value of the pressure coefficient.
Reimplemented from CSolver.
§ SetOmega_Max()
|
inlinevirtual |
§ SetPrimitive_Variables()
|
virtual |
Compute the velocity^2, SoundSpeed, Pressure, Enthalpy, Viscosity.
- Parameters
-
[in] solver_container - Container vector with all the solutions. [in] config - Definition of the particular problem. [in] Output - boolean to determine whether to print output.
- Returns
- - The number of non-physical points.
Reimplemented from CEulerSolver.
§ SetStrainMag_Max()
|
inlinevirtual |
§ SetTime_Step()
|
virtual |
Compute the time step for solving the Navier-Stokes equations with turbulence model.
- Parameters
-
[in] geometry - Geometrical definition of the problem. [in] solver_container - Container vector with all the solutions. [in] config - Definition of the particular problem. [in] iMesh - Index of the mesh in multigrid computations. [in] Iteration - Index of the current iteration.
Reimplemented from CEulerSolver.
§ Viscous_Residual()
|
virtual |
Compute the viscous residuals.
- Parameters
-
[in] geometry - Geometrical definition of the problem. [in] solver_container - Container vector with all the solutions. [in] numerics - Description of the numerical method. [in] config - Definition of the particular problem. [in] iMesh - Index of the mesh in multigrid computations. [in] iRKStep - Current step of the Runge-Kutta iteration.
Reimplemented from CSolver.
The documentation for this class was generated from the following files:
- SU2_CFD/include/solver_structure.hpp
- SU2_CFD/include/solver_structure.inl
- SU2_CFD/src/solver_direct_mean.cpp
