Calculation of the flow past a delta wing in the thin shock layer approximation

DOI10.1016/0041-5553(89)90198-5zbMath0712.76060OpenAlexW2071130325MaRDI QIDQ3197543

V. V. Negoda, V. N. Golubkin

Publication date: 1989

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(89)90198-5

zbMATH Keywords

hypersonic flowflat delta wing of small aspect ratioshock layer method

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Transonic flows (76H05)

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