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Towards shock-stable and accurate hypersonic heating computations: A new pressure flux for AUSM-family schemes

Numerical AnalysisCompressible FlowEngineeringThermoacoustic Heat EngineAerospace EngineeringShock CompressionSupersonic CombustionHyperbolic Conservation LawNumerical SimulationNew Pressure FluxThermodynamicsHeat TransferHypersonic FlowThermal EngineeringAusm-family Schemes