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Aerodynamic shape optimization design of the swept wing based on the Kriging surrogate model

  • Northwestern Polytechnical University Xian
  • Chinese Aeronautical Establishment

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

The aerodynamic shape optimization design system was established in this paper. In the system, the RANS equation was used for solving the flowing; the free form deformation (FFD) method was used for the geometry parameterization, and the genetic algorithm was used for the optimization search. For the reducing of the time cost, the Kriging model was used for the surrogate model instead of the CFD simulation during the optimization design. The aerodynamic shape design of a swept wing was presented which used the system, and the result indicated that the 14% drag coefficient was reduced at the cruise conditions, which proved the validity of the system.

源语言英语
主期刊名Advances in Computational Modeling and Simulation
1277-1282
页数6
DOI
出版状态已出版 - 2014
活动2nd International Conference on Advances in Computational Modeling and Simulation, ACMS 2013 - Kunming, 中国
期限: 17 7月 201319 7月 2013

出版系列

姓名Applied Mechanics and Materials
444-445
ISSN(印刷版)1660-9336
ISSN(电子版)1662-7482

会议

会议2nd International Conference on Advances in Computational Modeling and Simulation, ACMS 2013
国家/地区中国
Kunming
时期17/07/1319/07/13

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