Calculation of supersonic flow past the weather side of a wing of small aspect ratio at large angles of attack

DOI10.1016/0041-5553(88)90034-1zbMath0702.76070OpenAlexW2085478318MaRDI QIDQ3481393

V. V. Negoda, V. N. Golubkin

Publication date: 1988

Published in: USSR Computational Mathematics and Mathematical Physics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0041-5553(88)90034-1

zbMATH Keywords

asymptotic methodsupersonic flowinverse flow problemthree- dimensional flowcompressed gas flowthin wing of small aspect ratiotwo- layer structure

Mathematics Subject Classification ID

Supersonic flows (76J20)

Related Items (2)

An inverse problem for determining the shape of the wedge in steady supersonic potential flow ⋮ Three-dimensional hypersonic gas flow over wings

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