A finite difference scheme for steady, supersonic, two-dimensional, compressible flow of real gases

DOI10.1016/0898-1221(92)90006-4zbMath0763.76048OpenAlexW2009792435MaRDI QIDQ1205903

P. Glaister

Publication date: 1 April 1993

Published in: Computers \& Mathematics with Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0898-1221(92)90006-4

zbMATH Keywords

shock-capturingspace-marchingoblique hydraulic jumpsnumerical characteristic decompositionreflection from a wall

Mathematics Subject Classification ID

Finite difference methods applied to problems in fluid mechanics (76M20) Gas dynamics (general theory) (76N15)

Related Items (2)

A weak formulation of Roe's scheme for two-dimensional, unsteady, compressible flows and steady, supersonic flows ⋮ A comparison of the different extensions of a weak formulation of an approximate Riemann solver for supercritical flows and their relationship to existing schemes

Cites Work

• Unnamed Item
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• An approximate linearised Riemann solver for the Euler equations for real gases
• Numerical calculations of steady three-dimensional turbulent jets in cross flow
• An efficient Riemann solver for unsteady flows with non-ideal gases
• High Resolution Schemes Using Flux Limiters for Hyperbolic Conservation Laws

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