Multiobjective genetic algorithm for multidisciplinary design of transonic wing planform

Shigeru Obayashi, Yoshihiro Yamaguchi, Takashi Nakamura

Research output: Contribution to journalArticlepeer-review

80 Citations (Scopus)

Abstract

A multiobjective genetic algorithm based on Pareto ranking is applied to the multidisciplinary optimization of a transonic wing planform. The method is implemented at the numerical wind tunnel using the master-slave concept. Planform shapes with minimum drag, minimum weight, and maximum fuel weight, under constraints of lift and structural strength are determined by using the analysis model FLO22 that consisted of potential flow, algebraic weight, and wing-box structure equations. A wide variety of Pareto solutions are obtained, including a good compromised solution.

Original languageEnglish
Pages (from-to)690-692
Number of pages3
JournalJournal of Aircraft
Volume34
Issue number5
DOIs
Publication statusPublished - 1997 Jan 1

ASJC Scopus subject areas

  • Aerospace Engineering

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