Euler/Navier-Stokes optimization of supersonic wing design based on evolutionary algorithm

Akira Oyama, Shigeru Obayashi, Kazuhiro Nakahashi, Takashi Nakamura

Research output: Contribution to journalArticlepeer-review

14 Citations (Scopus)

Abstract

An evolutionary algorithm (EA) coupled with a Euler/Navier-Stokes code has been applied to supersonic wing shape design. Aerodynamic evaluations are distributed to the processing elements (PE) of the numerical wind tunnel (NWT) to overcome the enormous computational time necessary for the optimization. The design yields both the minimum drag and the minimum volume wave drag in the given design space. The important features of supersonic wing design as compared with conventional transonic wing design are presented.

Original languageEnglish
Pages (from-to)1327-1328
Number of pages2
JournalAIAA journal
Volume37
Issue number10
DOIs
Publication statusPublished - 1999 Oct

ASJC Scopus subject areas

  • Aerospace Engineering

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