Approximate solutions for oblique detonations in the hypersonic limit

DOI10.2514/3.10978zbMath0766.76096OpenAlexW2115470588MaRDI QIDQ4036316

Joseph M. Powers, D. Scott Stewart

Publication date: 16 May 1993

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: https://semanticscholar.org/paper/97ff65677c409a6c7cf67cf2b0c904bd2cd00eef

zbMATH Keywords

wedgere-entry vehicleshypersonic airframesirrotational flowfieldpremixed reactive ideal gasRankine-Hugoniot theoryrotational flowfieldstraight shock

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Reaction effects in flows (76V05) Hypersonic flows (76K05)

Related Items (4)

Wave angle for oblique detonation waves ⋮ Numerical predictions of oblique detonation stability boundaries ⋮ Reaction zone structure for strong, weak overdriven, and weak underdriven oblique detonations ⋮ Morphology of oblique detonation waves in a stoichiometric hydrogen–air mixture

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