Turbulent boundary layer behind constant velocity shock including wall blowing effects

DOI10.2514/3.8736zbMath0553.76057OpenAlexW2128522350MaRDI QIDQ3216334

Harold Mirels

Publication date: 1984

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

Full work available at URL: https://doi.org/10.2514/3.8736

zbMATH Keywords

shock moving with uniform speedwall ablation

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Turbulence (76F99) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

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