48 STATE
Enthalpy(STATE soundSpeed, STATE speed);
52 STATE &
Speed, STATE &NormalSpeed, STATE &
Enthalpy, STATE &press);
55 STATE
FacePressure(STATE pL, STATE pR, STATE Ml, STATE Mr);
61 STATE
NumSoundSpeed(STATE LeftSoundSpeed,STATE RightSoundSpeed);
64 STATE
MassFlux(STATE NumericalSoundSpeed, STATE rhoL, STATE rhoR, STATE FaceMach);
STATE fAlpha
Method constants.
TPZAUSMFlux(STATE gamma)
Constructor with Gamma value.
STATE Speed(TPZVec< STATE > &sol, TPZVec< REAL > &normal, STATE &NormalSpeed)
Returns speed.
Templated vector implementation.
void ComputeInitialData(TPZVec< STATE > &sol, TPZVec< REAL > &normal, STATE &soundSpeed, STATE &Speed, STATE &NormalSpeed, STATE &Enthalpy, STATE &press)
Auxiliar method only.
STATE Enthalpy(STATE soundSpeed, STATE speed)
Returns enthalpy.
STATE FacePressure(STATE pL, STATE pR, STATE Ml, STATE Mr)
Returns pressure in the face.
Contains TPZMatrixclass which implements full matrix (using column major representation).
STATE MassFlux(STATE NumericalSoundSpeed, STATE rhoL, STATE rhoR, STATE FaceMach)
Returns the mass flux.
long double gamma(unsigned int n)
Evaluate the factorial of a integer.
void ComputeFlux(TPZVec< STATE > &solL, TPZVec< STATE > &solR, TPZVec< REAL > &normal, TPZVec< STATE > &F)
Computes numerical flux.
STATE SoundSpeed(TPZVec< STATE > &sol, STATE press)
Returns sound speed.
STATE NumSoundSpeed(STATE LeftSoundSpeed, STATE RightSoundSpeed)
Computes the numerical sound speed at the face.
STATE FaceMachNumber(STATE Ml, STATE Mr)
Returns mach number in the face.
STATE fGamma
Ratio between specific heat is constant and the specific heat the constant volume of a polytropic gas...
Contains the declaration of TPZFlopCounter class and TPZCounter struct.
STATE Pressure(TPZVec< STATE > &sol)
Returns pressure values.
Implements the numerical flux for AUSM problem. (Jorge?)