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Progress in design optimization using evolutionary algorithms for aerodynamic problems

期刊

PROGRESS IN AEROSPACE SCIENCES
卷 46, 期 5-6, 页码 199-223

出版社

PERGAMON-ELSEVIER SCIENCE LTD
DOI: 10.1016/j.paerosci.2009.08.003

关键词

Multi-objective design optimization; Evolutionary algorithms; Surrogate model; Robust and reliability-based design; Data mining; NASA rotor 67 blade

资金

  1. NASA [NAG3-2869]
  2. Subsonic Fixed Wing Project

向作者/读者索取更多资源

Evolutionary algorithms (EAs) are useful tools in design optimization. Due to their simplicity, ease of use, and suitability for multi-objective design optimization problems, EAs have been applied to design optimization problems from various areas. In this paper we review the recent progress in design optimization using evolutionary algorithms to solve real-world aerodynamic problems. Examples are given in the design of turbo pump, compressor, and micro-air vehicles. The paper covers the following topics that are deemed important to solve a large optimization problem from a practical viewpoint: (1) hybridized approaches to speed up the convergence rate of EAs; (2) the use of surrogate model to reduce the computational cost stemmed from EAs; (3) reliability based design optimization using EAs; and (4) data mining of Pareto-optimal solutions. Published by Elsevier Ltd.

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