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Numerical research on separated flow around a WIG craft in flight close to ground at high incidence angle

  • Qiu Lin Qu*
  • , Pei Qing Liu
  • , Xu Guo Qin
  • *此作品的通讯作者
  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

Numerical results are presented by simulating the separated flow around a WIG craft in flight close to ground at a high incidence angle. The Farve-averaged N-S equation of steady compressible flow and the standard k-ε turbulence model are solved by Fluent software. The effects of flight height on the separated flow a-round wings of WIG craft are provided. Why flow separates at lower flight height is explained. The effects of the separated flow on aerodynamics of WIG craft are analyzed in detail.

源语言英语
页(从-至)72-77
页数6
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
28
1
出版状态已出版 - 1月 2007

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