Design and optimization of a two-element wing airfoil in a subsonic viscous flow

DOI10.1007/s10697-006-0018-yzbMath1198.76121OpenAlexW2020098223MaRDI QIDQ604567

N. B. Il'yinskij, P. A. Volkov

Publication date: 11 November 2010

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

Full work available at URL: https://doi.org/10.1007/s10697-006-0018-y

zbMATH Keywords

optimizationChaplygin gasboundary layerinverse boundary-value problems of aerohydrodynamicstwo element wing airfoil

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Uses Software

• Spalart-Allmaras

Cites Work

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• Solution of the inverse boundary value problem of aerohydrodynamics for a two-element airfoil

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