Lifting wings of optimum shape in a viscous hypersonic stream

DOI10.1007/BF02078211zbMath0861.76074OpenAlexW2034927609MaRDI QIDQ1925307

V. N. Golubkin

Publication date: 21 May 1997

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

Full work available at URL: https://doi.org/10.1007/bf02078211

zbMATH Keywords

bifurcationboundary layerpressure distributionsnumerical-analytic solutioninfluence of viscositymaximum lift-to-drag ratiolow-aspect-ratio wing

Mathematics Subject Classification ID

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

Related Items (4)

Comments on the choice of waverider shape ⋮ Lift-drag ratio of a hypersonic waverider of delta planform ⋮ Waveriders of complicated shape ⋮ Optimization of the shape of a wing in a hypersonic nonequilibrium gas flow

Uses Software

• TsAGI

Cites Work

• Unnamed Item
• 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
• Improving the aerodynamic performance of small-aspect-ratio wings at hypersonic speeds
• Aerodynamic characteristics of \(V\)-shaped wings with shock waves detached from leading edges at hypersonic speeds
• Three-dimensional hypersonic gas flow over wings
• Optimizing hypersonic wings
• Three-dimensional wings and waveriders with attached shock waves
• LIFT OF SLENDER DELTA WINGS ACCORDING TO NEWTONIAN THEORY

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