Minimization of the wing airfoil drag coefficient using the optimal control method

DOI10.1007/s10697-006-0013-3zbMath1198.76116OpenAlexW1969286542MaRDI QIDQ604429

D. F. Abzalilov

Publication date: 10 November 2010

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

Full work available at URL: https://doi.org/10.1007/s10697-006-0013-3

zbMATH Keywords

optimal controldragaerodynamicswing airfoilboundary layer suction

Mathematics Subject Classification ID

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

Related Items (1)

An inverse problem for determining the shape of the wedge in steady supersonic potential flow

Cites Work

• Unnamed Item
• Optimum suction distribution for transition control
• Methods of non-local improvement for admissible controls in linear problems with delay
• Optimal control with singular regions

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