Hypersonic flow past a delta wing

DOI10.1016/0021-8928(70)90091-2zbMath0267.76046OpenAlexW1635190757MaRDI QIDQ2562737

A. L. Gonor

Publication date: 1970

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(70)90091-2

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Related Items (4)

Hypersonic flow past delta wing of finite thickness ⋮ Hypersonic flow past an airfoil with a Mach system of shock waves ⋮ Aerodynamic characteristics of \(V\)-shaped wings with shock waves detached from leading edges at hypersonic speeds ⋮ Three-dimensional hypersonic gas flow over wings

Cites Work

• Unnamed Item
• Supersonic flow past triangular wings with ribs on their surface
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY

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