Numerical method and results for inviscid supersonic flow over a compressive ramp

DOI10.1016/0045-7930(83)90021-XzbMath0529.76060OpenAlexW2041912043MaRDI QIDQ787792

George Emanuel

Publication date: 1983

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

Full work available at URL: https://doi.org/10.1016/0045-7930(83)90021-x

zbMATH Keywords

algorithmweak solutionstrong solutionoblique shocktwo-dimensionalinviscidsteadyslipstreamcentered, Prandtl-Meyer compressionsecondary disturbancewall with compressive turn

Mathematics Subject Classification ID

Supersonic flows (76J20) Basic methods in fluid mechanics (76M99)

Related Items (1)

Transitions of shock interactions on V-shaped blunt leading edges

Cites Work

• Stability of Shock Waves Attached to Wedges and Cones

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