Numerical study of steady supersonic separated flow past spatial lifting systems

DOI10.1007/BF01051157zbMath0793.76062OpenAlexW2005777825MaRDI QIDQ1316781

S. S. Gras'kin

Publication date: 12 April 1994

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf01051157

zbMATH Keywords

wingsvortex elementsvortex filaments

Mathematics Subject Classification ID

Supersonic flows (76J20)

Cites Work

• Method of calculating subsonic gas flow with separation past wings

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