Hypersonic flow past conical V-shaped wings

DOI10.1007/BF02078231zbMath0888.76040MaRDI QIDQ1375306

V. N. Golubkin

Publication date: 14 January 1998

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

zbMATH Keywords

thin shock layer methodconical flow patternsdelta wings

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Cites Work

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• Aerodynamic characteristics of \(V\)-shaped wings with shock waves detached from leading edges at hypersonic speeds
• Hypersonic flow past an airfoil with a Mach system of shock waves
• Hypersonic flow past delta wing of finite thickness
• Hypersonic flow with attached shock waves over plane delta wings
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY

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