Method of calculating subsonic gas flow with separation past wings

DOI10.1007/BF01091090zbMath0566.76059OpenAlexW2028036532MaRDI QIDQ1059482

S. M. Belotserkovskij, V. N. Korzhnev, S. D. Shipilov

Publication date: 1984

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

Full work available at URL: https://doi.org/10.1007/bf01091090

zbMATH Keywords

compressible gasmethod of discrete vorticessteady nonlinear problemwing of arbitrary shape

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Gas dynamics (general theory) (76N15) Basic methods in fluid mechanics (76M99)

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Numerical study of steady supersonic separated flow past spatial lifting systems

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