Genetic optimization of target pressure distributions for inverse design methods

Shigeru Obayashi, Susumu Takanashi

研究成果: Paper査読

7 被引用数 (Scopus)

抄録

A Genetic Algorithm (GA) has been applied to optimize target pressure distributions for 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/wing geometries can be computed by an inverse design code coupled with a Navier-Stokes solver. Design examples indicate that the present optimization algorithm is efficient and that supercritical wing shapes are reproduced by the simulated evolution.

本文言語English
ページ33-42
ページ数10
DOI
出版ステータスPublished - 1995
イベント12th Computational Fluid Dynamics Conference, 1995 - San Diego, United States
継続期間: 1995 6 191995 6 22

Other

Other12th Computational Fluid Dynamics Conference, 1995
国/地域United States
CitySan Diego
Period95/6/1995/6/22

ASJC Scopus subject areas

  • 工学(全般)

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