Home
last modified time | relevance | path

Searched refs:HeatCapacityRatio (Results 1 – 9 of 9) sorted by relevance

/honee/qfunctions/
H A Dnewtonian_state.h42 CEED_QFUNCTION_HELPER CeedScalar HeatCapacityRatio(NewtonianIGProperties gas) { return gas.cp / gas… in HeatCapacityRatio() function
48 …ed(NewtonianIGProperties gas, CeedScalar T) { return sqrt(gas.cp * (HeatCapacityRatio(gas) - 1.) *… in SoundSpeed()
71 Y.pressure = (HeatCapacityRatio(gas) - 1) * U.density * e_internal; in StatePrimitiveFromConservative()
87 …dY.pressure = (HeatCapacityRatio(gas) - 1) * (dU.density * e_internal + s.U.density * d… in StatePrimitiveFromConservative_fwd()
93 const CeedScalar gamma = HeatCapacityRatio(gas); in StateEntropyFromPrimitive()
107 const CeedScalar gamma = HeatCapacityRatio(gas); in StateEntropyFromPrimitive_fwd()
127 const CeedScalar gamma = HeatCapacityRatio(gas); in StatePrimitiveFromEntropy()
140 const CeedScalar gamma = HeatCapacityRatio(gas); in StatePrimitiveFromEntropy_fwd()
177 const CeedScalar gamma = HeatCapacityRatio(gas); in StateEntropyFromConservative()
191 const CeedScalar gamma = HeatCapacityRatio(gas); in StateEntropyFromConservative_fwd()
[all …]
H A Dgaussianwave.h35 const CeedScalar gamma = HeatCapacityRatio(gas); in IC_GaussianWave()
H A Dchannel.h87 const CeedScalar gamma = HeatCapacityRatio(gas); in Channel_Inflow()
H A Driemann_solver.h99 const CeedScalar gamma = HeatCapacityRatio(gas); in ComputeHLLSpeeds_Roe()
120 const CeedScalar gamma = HeatCapacityRatio(gas); in ComputeHLLSpeeds_Roe_fwd()
H A Dstg_shur14.h353 const CeedScalar gamma = HeatCapacityRatio(gas); in StgShur14Inflow()
424 const CeedScalar gamma = HeatCapacityRatio(gas); in StgShur14Inflow_Jacobian()
H A Dblasius.h187 const CeedScalar gamma = HeatCapacityRatio(gas); in Blasius_Inflow_Jacobian()
/honee/problems/
H A Dbc_freestream.c222 const CeedScalar p = (HeatCapacityRatio(gas) - 1) * rho * gas.cv * T; in TestRiemannHLL_fwd()
284 const CeedScalar p = (HeatCapacityRatio(gas) - 1) * rho * gas.cv * T; in TestRiemannHLLC_fwd()
346 const CeedScalar p = (HeatCapacityRatio(gas) - 1) * rho * gas.cv * T; in TestComputeHLLSpeeds_Roe_fwd()
421 const CeedScalar p = (HeatCapacityRatio(gas) - 1) * rho * gas.cv * T; in TestTotalSpecificEnthalpy_fwd()
H A Dblasius.c27 … Ma = Mach(gas, S_infty.Y.temperature, U_infty), Pr = Prandtl(gas), gamma = HeatCapacityRatio(gas); in CompressibleBlasiusResidual()
H A Dnewtonian.c741 const CeedScalar P = (HeatCapacityRatio(gas) - 1) * rho * gas.cv * T; in UnitTests_Newtonian()
747 const CeedScalar gamma = HeatCapacityRatio(gas); in UnitTests_Newtonian()