On the role of a balancing load in the problem of aerodynamic drag minimization in the supersonic flight regime

DOI10.1134/S0015462814020124zbMath1294.76216MaRDI QIDQ404055

S. A. Takovitskij

Publication date: 29 August 2014

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

zbMATH Keywords

optimizationbalancingaircraftwingaerodynamic dragairfoildead loadsupersonic flight

Mathematics Subject Classification ID

Supersonic flows (76J20) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Cites Work

• Design of the optimal nozzle of a hypersonic flight vehicle for given overall dimensions and moment
• Analytic solution in the problem of constructing an airfoil with minimum wave drag

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