Optimization of the shape of a wing in a hypersonic nonequilibrium gas flow

DOI10.1007/BF02831438zbMath0992.76079OpenAlexW2068092594MaRDI QIDQ1592074

V. N. Golubkin, D. S. Postnov

Publication date: 11 September 2002

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

Full work available at URL: https://doi.org/10.1007/bf02831438

zbMATH Keywords

nonequilibrium flowmaximum lift-to-drag ratiooptimal low-aspect-ratio wingreal-gas effectterrestrial atmosphere conditions

Mathematics Subject Classification ID

Variational methods applied to problems in fluid mechanics (76M30) Hypersonic flows (76K05) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Cites Work

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• Hypersonic flow past a wing at large angles of attack with detached shock wave
• Optimization of the spatial shape of load-carrying bodies of small elongation at hypersonic velocities
• Calculation of the maximum hypersonic fineness ratio and optimal configuration of short-span wings with laminar and turbulent boundary layers.
• Optimum lifting body shapes in hypersonic flow at high angles of attack
• Lifting wings of optimum shape in a viscous hypersonic stream
• Nonequilibrium flow over delta wings with detached shock waves
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY

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