Supersonic flow over a rearward facing step with transverse nonreacting hydrogen injection

DOI10.2514/3.8313zbMath0542.76156OpenAlexW1969642552MaRDI QIDQ3330884

J. Philip Drummond, Harry A. Berman, John D. jun. Anderson

Publication date: 1983

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

Full work available at URL: https://doi.org/10.2514/3.8313

zbMATH Keywords

turbulentrearward-facing stepsupersonic combustion ramjet enginetime-dependent, finite difference methodtransverse \(H_ 2\) injectiontwo-dimensional Reynolds averaged Navier-Stokes equations

Mathematics Subject Classification ID

Combustion (80A25) Reaction effects in flows (76V05) Basic methods in fluid mechanics (76M99)

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