Multi-objective aerodynamic optimization of sweptwing

Ling Tao Meng*, Li Liu, Teng Long, Hua Guang Zhu

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

Abstract

Taking sweptwing as example of aerodynamic optimization, integration framework of aerodynamic was built based on Model Center software with VB program, CAD, CFD software and genetic algorithm. Two kinds of optimization projects, Multi-objective Genetic Algorithm associate with three-dimensional CFD and response surface models (RSM) respectively, were used in the optimization process. The result of two projects associating with analysis of flow field demonstrates feasibility and robustness of those projects for aerodynamic optimization design and integration framework.

Original languageEnglish
Pages (from-to)1033-1036+1039
JournalXitong Fangzhen Xuebao / Journal of System Simulation
Volume21
Issue number4
Publication statusPublished - 20 Feb 2009

Keywords

  • CFD
  • Genetic algorithm
  • Integration framework
  • Multi-objective aerodynamic optimization design
  • RSM

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