Response surface approach to aerodynamic optimization design of helicopter rotor blade

DOI10.1002/nme.1391zbMath1108.76354OpenAlexW1970632976MaRDI QIDQ5695887

Soogab Lee, Hyosung Sun

Publication date: 6 October 2005

Published in: International Journal for Numerical Methods in Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1002/nme.1391

zbMATH Keywords

regression analysisanalysis of variancegenetic algorithm (ga)multi-disciplinary design optimization (mdo)response surface method (rsm)

Mathematics Subject Classification ID

Transonic flows (76H05) General aerodynamics and subsonic flows (76G25) Flow control and optimization for compressible fluids and gas dynamics (76N25)

Related Items (1)

2D shape optimization under proximity constraints by CFD and response surface methodology

Cites Work

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