Optimum lifting body shapes in hypersonic flow at high angles of attack

DOI10.1007/BF00312398zbMath0822.76050OpenAlexW2033389581MaRDI QIDQ1892186

V. N. Golubkin, V. V. Negoda

Publication date: 8 June 1995

Published in: Theoretical and Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00312398

zbMATH Keywords

bifurcationmaximum lift-to-drag ratiominimization of linear functionalnonequilibrium thermochemical effectsthin shock-layer theoryviscous drag effects

Mathematics Subject Classification ID

Variational methods applied to problems in fluid mechanics (76M30) Hypersonic flows (76K05)

Related Items (1)

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

Cites Work

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• Nonequilibrium hypersonic flow of gas past a wing of small aspect ratio
• Calculation of the flow past a delta wing in the thin shock layer approximation
• Nonequilibrium flow over delta wings with detached shock waves
• Hypersonic flow with attached shock waves over plane delta wings
• A wing with the maximum lift/drag ratio at supersonic velocity
• A class of three-dimensional, optimum hypersonic wings.
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY

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