An effective flux scheme for hypersonic heating prediction of re-entry vehicles

DOI10.1016/j.compfluid.2018.05.028zbMath1410.76265OpenAlexW2803434833WikidataQ129766645 ScholiaQ129766645MaRDI QIDQ1625635

Feng Qu, Chao Yan, Di Sun

Publication date: 29 November 2018

Published in: Computers and Fluids (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.compfluid.2018.05.028

zbMATH Keywords

Navier-Stokes equationscomputational fluid dynamicsall speedshypersonic aeroheating predictionre-entry vehicles

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Hypersonic flows (76K05) Finite volume methods for initial value and initial-boundary value problems involving PDEs (65M08) Compressible fluids and gas dynamics (76Nxx)

Related Items (3)

Mixing enhancement of a compressible jet over a convex wall ⋮ Unified stochastic particle simulation of polyatomic gas flows using SPARTACUS ⋮ Numerical study of instabilities and compressibility effects on supersonic jet over a convex wall

Uses Software

• AUSM
• HE-E1GODF
• FLICA-OVAP

Cites Work

• Towards shock-stable and accurate hypersonic heating computations: a new pressure flux for AUSM-family schemes
• A sequel to AUSM: AUSM\(^ +\)
• Approximate Riemann solvers, parameter vectors, and difference schemes
• Towards the ultimate conservative difference scheme. IV: A new approach to numerical convection
• A new flux splitting scheme for the Euler equations
• Assessment of SLAU2 and other flux functions with slope limiters in hypersonic shock-interaction heating
• Mechanism of Roe-type schemes for all-speed flows and its application
• Flux splitting schemes for the Euler equations
• Numerical and experimental investigation of oblique shock wave reflection off a water wedge
• CRITICAL HYPERSONIC AEROTHERMODYNAMIC PHENOMENA
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