Transonic wing shape optimization based on evolutionary algorithms

Shigeru Obayashi, Akira Oyama, Takashi Nakamura

Research output: Chapter in Book/Report/Conference proceedingConference contribution

4 Citations (Scopus)

Abstract

A practical three-dimensional shape optimization for aerodynamic design of a transonic wing has been performed using Evolutionary Algorithms (EAs). Because EAs coupled with aerodynamic function evaluations require enormous computational time, Numerical Wind Tunnel (NWT) located at National Aerospace Laboratory in Japan has been utilized based on the simple master-slave concept. Parallel processing makes EAs a very promising approach for practical aerodynamic design.

Original languageEnglish
Title of host publicationHigh Performance Computing - 3rd International Symposium, ISHPC 2000, Proceedings
EditorsMateo Valero, Kazuki Joe, Masaru Kitsuregawa, Hidehiko Tanaka
PublisherSpringer Verlag
Pages172-181
Number of pages10
ISBN (Print)9783540411284
DOIs
Publication statusPublished - 2000
Event3rd International Symposium on High Performance Computing, ISHPC 2000 - Tokyo, Japan
Duration: 2000 Oct 162000 Oct 18

Publication series

NameLecture Notes in Computer Science (including subseries Lecture Notes in Artificial Intelligence and Lecture Notes in Bioinformatics)
Volume1940
ISSN (Print)0302-9743
ISSN (Electronic)1611-3349

Other

Other3rd International Symposium on High Performance Computing, ISHPC 2000
CountryJapan
CityTokyo
Period00/10/1600/10/18

ASJC Scopus subject areas

  • Theoretical Computer Science
  • Computer Science(all)

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