Computation of non-equilibrium hypersonic flow with artificially upstream flux vector splitting (AUFS) schemes

DOI10.1080/10618560701766525zbMath1184.76757OpenAlexW2045066992MaRDI QIDQ3551629

Ghislain Tchuen, Yves Burtschell, David E. Zeitoun

Publication date: 15 April 2010

Published in: International Journal of Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1080/10618560701766525

zbMATH Keywords

hypersonic flowupwind solversartificially upstream flux vector splitting (AUFS)thermochemical non-equilibrium flow

Mathematics Subject Classification ID

Finite volume methods applied to problems in fluid mechanics (76M12) Reaction effects in flows (76V05) Hypersonic flows (76K05)

Related Items (5)

On two deficiencies of the AUFS scheme for Euler flows and possible fixes ⋮ A hybrid numerical method and its application to inviscid compressible flow problems ⋮ Evaluation of Euler fluxes by a high-order CFD scheme: shock instability ⋮ Numerical study of the interaction of type IVr around a double-wedge in hypersonic flow ⋮ An accurate shock-capturing scheme based on rotated-hybrid Riemann solver

Uses Software

• HE-E1GODF

Cites Work

• Unnamed Item
• Flux-split algorithms for the multi-dimensional Euler equations with real gases
• Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methods
• Approximate Riemann solvers, parameter vectors, and difference schemes
• A new flux splitting scheme
• An artificially upstream flux vector splitting scheme for the Euler equations.
• An improvement of AUSM schemes by introducing the pressure-based weight functions
• On Upstream Differencing and Godunov-Type Schemes for Hyperbolic Conservation Laws
• Numerical Solutions of Supersonic and Hypersonic Laminar Compression Corner Flows
• Vibrational nonequilibrium effects on diatomic dissociation rates

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