Hypersonic calculations by Riemann solvers techniques

DOI10.1016/0010-4655(91)90148-EzbMath0900.76228OpenAlexW2011175427MaRDI QIDQ1365945

Remi Abgrall

Publication date: 30 March 1998

Published in: Computer Physics Communications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0010-4655(91)90148-e

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Hypersonic flows (76K05)

Related Items (1)

An extension of Osher's Riemann solver for chemical and vibrational non-equilibrium gas flows

Cites Work

• Inviscid flux-splitting algorithms for real gases with non-equilibrium chemistry
• Flux-split algorithms for flows with non-equilibrium chemistry and vibrational relaxation
• Nonequilibrium flow computations. I: An analysis of numerical formulations of conservation laws
• A class of implicit upwind schemes for Euler simulations with unstructured meshes
• Approximate Riemann solvers, parameter vectors, and difference schemes
• An extension of Roe's upwind scheme to algebraic equilibrium real gas models
• Numerical Experiments with the Osher Upwind Scheme for the Euler Equations
• Upwind Difference Schemes for Hyperbolic Systems of Conservation Laws
• An extension of Osher's Riemann solver for chemical and vibrational non-equilibrium gas flows

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