Genetic algorithm for aerodynamic inverse optimization problems

Shigeru Obayashi, Susumu Takanashi

研究成果: Conference article査読

19 被引用数 (Scopus)

抄録

A Genetic Algorithm (GA) has been applied to optimize target pressure distributions for aerodynamic inverse design methods. Since GAs do not require any derivative information, the resulting aerodynamic optimization algorithm is robust. Once target pressure distributions are obtained, corresponding airfoil geometries can be computed by an inverse design code using a Navier-Stokes solver. Design samples indicate that supercritical airfoil shapes are reproduced by the simulated evolution of a GA.

本文言語English
ページ(範囲)7-12
ページ数6
ジャーナルIEE Conference Publication
414
出版ステータスPublished - 1995 1月 1
イベントProceedings of the 1st IEE/IEEE International Conference on Genetic Algorithms in Engineering Systems: Innovations and Applications GALESIA '95 - Sheffield, Engl
継続期間: 1995 9月 121995 9月 14

ASJC Scopus subject areas

  • 電子工学および電気工学

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