#include <GodunovPhysics.H>
Collaboration diagram for GodunovPhysics:

Public Member Functions | |
| GodunovPhysics () | |
| Constructor. | |
| PhysIBC * | getPhysIBC () const |
| Get the initial and boundary condition object. | |
| void | setPhysIBC (PhysIBC *a_bc) |
| Set the initial and boundary condition object. | |
| virtual | ~GodunovPhysics () |
| Destructor. | |
| virtual void | define (const ProblemDomain &a_domain, const Real &a_dx) |
| Define the object. | |
| virtual void | setCurrentBox (const Box &a_currentBox) |
| Set the current box (default implementation - do nothing). | |
| virtual Real | getMaxWaveSpeed (const FArrayBox &a_U, const Box &a_box)=0 |
| Compute the maximum wave speed. | |
| virtual GodunovPhysics * | new_godunovPhysics () const=0 |
| Object factory for this class. | |
| virtual int | numConserved ()=0 |
| Number of conserved variables. | |
| virtual Vector< string > | stateNames ()=0 |
| Names of the conserved variables. | |
| virtual int | numFluxes ()=0 |
| Number of flux variables. | |
| virtual void | computeUpdate (FArrayBox &a_dU, FluxBox &a_F, const FArrayBox &a_U, const FluxBox &a_WHalf, const bool &a_useArtificialViscosity, const Real &a_artificialViscosity, const Real &a_currentTime, const Real &a_dx, const Real &a_dt, const Box &a_box) |
| Compute the increment in the conserved variables from face variables. | |
| virtual void | getFlux (FArrayBox &a_flux, const FArrayBox &a_WHalf, const int &a_dir, const Box &a_box) |
| Compute the fluxes from primitive variable values on a face. | |
| virtual bool | isDefined () const |
| Is the object completely defined. | |
| virtual int | numPrimitives ()=0 |
| Number of primitive variables. | |
| virtual void | charAnalysis (FArrayBox &a_dW, const FArrayBox &a_W, const int &a_dir, const Box &a_box)=0 |
| Transform a_dW from primitive to characteristic variables. | |
| virtual void | charSynthesis (FArrayBox &a_dW, const FArrayBox &a_W, const int &a_dir, const Box &a_box)=0 |
| Transform a_dW from characteristic to primitive variables. | |
| virtual void | charValues (FArrayBox &a_lambda, const FArrayBox &a_W, const int &a_dir, const Box &a_box)=0 |
| Compute the characteristic values (eigenvalues). | |
| virtual void | incrementSource (FArrayBox &a_S, const FArrayBox &a_W, const Box &a_box)=0 |
| Add to (increment) the source terms given the current state. | |
| virtual void | riemann (FArrayBox &a_WStar, const FArrayBox &a_WLeft, const FArrayBox &a_WRight, const FArrayBox &a_W, const Real &a_time, const int &a_dir, const Box &a_box)=0 |
| Compute the solution to the Riemann problem. | |
| virtual void | postNormalPred (FArrayBox &a_dWMinus, FArrayBox &a_dWPlus, const FArrayBox &a_W, const Real &a_dt, const Real &a_dx, const int &a_dir, const Box &a_box)=0 |
| Post-normal predictor calculation. | |
| virtual void | quasilinearUpdate (FArrayBox &a_AdWdx, const FArrayBox &a_wHalf, const FArrayBox &a_W, const Real &a_scale, const int &a_dir, const Box &a_box)=0 |
| Compute the quasilinear update A*dW/dx. | |
| virtual void | consToPrim (FArrayBox &a_W, const FArrayBox &a_U, const Box &a_box)=0 |
| Compute primitive variables from conserved variables. | |
| virtual Interval | velocityInterval ()=0 |
| Interval within the primitive variables corresponding to the velocities. | |
| virtual int | pressureIndex ()=0 |
| Component index within the primitive variables of the pressure. | |
| virtual Real | smallPressure ()=0 |
| Used to limit the absolute value of a "pressure" difference. | |
| virtual int | bulkModulusIndex ()=0 |
| Component index within the primitive variables of the bulk modulus. | |
| virtual void | artVisc (FArrayBox &a_F, const FArrayBox &a_U, const Real &a_artificialViscosity, const Real &a_currentTime, const int &a_dir, const Box &a_box) |
| Compute the artificial viscosity contribution to the flux. | |
Protected Attributes | |
| bool | m_isDefined |
| ProblemDomain | m_domain |
| Real | m_dx |
| GodunovUtilities | m_util |
| PhysIBC * | m_bc |
| bool | m_isBCSet |
Private Member Functions | |
| void | operator= (const GodunovPhysics &a_input) |
| GodunovPhysics (const GodunovPhysics &a_input) | |
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Constructor.
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Destructor.
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Get the initial and boundary condition object.
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Set the initial and boundary condition object.
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Define the object.
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Set the current box (default implementation - do nothing).
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Compute the maximum wave speed.
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Object factory for this class.
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Number of conserved variables. Return the number of conserved variables. |
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Names of the conserved variables. Return the names of the conserved variables. |
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Number of flux variables. Return the number of flux variables. This can be greater than the number of conserved variables if addition fluxes/face-centered quantities are computed. |
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Compute the increment in the conserved variables from face variables. Compute dU = dt*dUdt, the change in the conserved variables over the time step. The fluxes are returned are suitable for use in refluxing. This has a default implementation but can be redefined as needed. |
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Compute the fluxes from primitive variable values on a face. This has a default implementation which throws an error. The method is here so that the default implementation of "computeUpdate" can use it and the user can supply it. It has an implementation so if the user redefines "computeUpdate" they aren't force to implement "getFlux" - which is only used by the default implementation of "computeUpdate". |
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Is the object completely defined. Return true if the object is completely defined. |
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Number of primitive variables. Return the number of primitive variables. This may be greater than the number of conserved variables if derived/redundant quantities are also stored for convenience. |
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Transform a_dW from primitive to characteristic variables. On input, a_dW contains the increments of the primitive variables. On output, it contains the increments in the characteristic variables. IMPORTANT NOTE: It is assumed that the characteristic analysis puts the smallest eigenvalue first, the largest eigenvalue last, and orders the characteristic variables accordingly. |
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Transform a_dW from characteristic to primitive variables. On input, a_dW contains the increments of the characteristic variables. On output, it contains the increments in the primitive variables. IMPORTANT NOTE: It is assumed that the characteristic analysis puts the smallest eigenvalue first, the largest eigenvalue last, and orders the characteristic variables accordingly. |
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Compute the characteristic values (eigenvalues). Compute the characteristic values (eigenvalues). IMPORTANT NOTE: It is assumed that the characteristic analysis puts the smallest eigenvalue first, the largest eigenvalue last, and orders the characteristic variables accordingly. |
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Add to (increment) the source terms given the current state. On input, a_S contains the current source terms. On output, a_S has had any additional source terms (based on the current state, a_W) added to it. This should all be done on the region defined by a_box. |
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Compute the solution to the Riemann problem. Given input left and right states in a direction, a_dir, compute a Riemann problem and generate fluxes at the faces within a_box. |
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Post-normal predictor calculation. Add increment to normal predictor, e.g. to account for source terms due to spatially-varying coefficients, to bound primitive variable ranges. |
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Compute the quasilinear update A*dW/dx.
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Compute primitive variables from conserved variables.
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Interval within the primitive variables corresponding to the velocities. Return the interval of component indices within the primitive variable of the velocities. Used for slope flattening (slope computation) and computing the divergence of the velocity (artificial viscosity). |
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Component index within the primitive variables of the pressure. Return the component index withn the primitive variables for the pressure. Used for slope flattening (slope computation). |
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Used to limit the absolute value of a "pressure" difference. Return a value that is used by slope flattening to limit (away from zero) the absolute value of a slope in the pressureIndex() component (slope computation). |
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Component index within the primitive variables of the bulk modulus. Return the component index withn the primitive variables for the bulk modulus. Used for slope flattening (slope computation) used as a normalization to measure shock strength. |
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Compute the artificial viscosity contribution to the flux. Compute the artificial viscosity contribution to the flux. This has a default implementation but this can be overridded as needed. |
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1.3.6