Three-dimensional hypersonic gas flow over wings

DOI10.1007/BF01051615zbMath0789.76061MaRDI QIDQ1317776

V. N. Golubkin

Publication date: 12 April 1994

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

zbMATH Keywords

thin shock layer method

Mathematics Subject Classification ID

Hypersonic flows (76K05)

Related Items

Development, current state of the art, and applications of local interaction theory. Review, Lifting wings of optimum shape in a viscous hypersonic stream, Singularities of the flow field in the neighborhood of the windward surface of a small aspect ratio delta wing in hypersonic stream

Cites Work

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• On the theory of a wing with small aspect ratio in a hypersonic flow
• Optimization of the spatial shape of load-carrying bodies of small elongation at hypersonic velocities
• Hypersonic flow past a delta wing
• Three-dimensional hypersonic gas flow past slender bodies at high angles of attack
• Calculation of supersonic flow past the weather side of a wing of small aspect ratio at large angles of attack
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY