Computational methods for shock waves in three-dimensional supersonic flow

DOI10.1016/0045-7825(91)90010-4zbMath0760.76061OpenAlexW2044305247MaRDI QIDQ1204211

Chien-peng Li

Publication date: 1 April 1993

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(91)90010-4

zbMATH Keywords

Euler equationsRiemann solvercentral artificial-viscosity and an upwind-biased difference methodsHermesshock fitting procedureShuttle

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Finite difference methods applied to problems in fluid mechanics (76M20) Supersonic flows (76J20)

Related Items (1)

Implicit finite volume methods and application to a delta wing problem

Cites Work

• Approximate Riemann solvers, parameter vectors, and difference schemes
• Towards the ultimate conservative difference scheme. IV: A new approach to numerical convection
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