A fully adaptive hybrid optimization of aircraft engine blades

DOI10.1016/J.CAM.2008.10.041zbMath1170.76047OpenAlexW2015652277MaRDI QIDQ837093

B. Druez, N. Lecerf, Laurent Dumas

Publication date: 10 September 2009

Published in: Journal of Computational and Applied Mathematics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.cam.2008.10.041

zbMATH Keywords

genetic algorithmslocal searchdescent methodglobal searchevolution strategy

Mathematics Subject Classification ID

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

Related Items (1)

Lipschitz gradients for global optimization in a one-point-based partitioning scheme

Cites Work

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• Hybrid method for aerodynamic shape optimization in automotive industry
• Viscous single and multicomponent airfoil design with genetic algorithms

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