Analytic solution in the problem of constructing an airfoil with minimum wave drag

DOI10.1023/B:FLUI.0000015235.61628.78zbMath1154.76375OpenAlexW2077301715MaRDI QIDQ2388101

S. A. Takovitskij

Publication date: 8 September 2005

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

Full work available at URL: https://doi.org/10.1023/b:flui.0000015235.61628.78

zbMATH Keywords

local analysisEuler model

Mathematics Subject Classification ID

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

Related Items (2)

Analytical solution in the problem of constructing axisymmetric noses with minimum wave drag ⋮ On the role of a balancing load in the problem of aerodynamic drag minimization in the supersonic flight regime

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