Hypersonic flow past a delta wing at large angles of attack

DOI10.1016/0021-8928(84)90131-XzbMath0575.76058OpenAlexW2091036539MaRDI QIDQ1064218

V. N. Golubkin

Publication date: 1985

Published in: Journal of Applied Mathematics and Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0021-8928(84)90131-x

zbMATH Keywords

attached shock waveflow past a delta wing of finite spanlarge angles of attackthin shock layer method

Mathematics Subject Classification ID

Shock waves and blast waves in fluid mechanics (76L05) Hypersonic flows (76K05)

Related Items (1)

Hypersonic flow past a wing at large angles of attack with detached shock wave

Cites Work

• Hypersonic flow past delta wing of finite thickness
• Nonlinear conical flow of a gas
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY
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