跳到主要导航 跳到搜索 跳到主要内容

Detached-eddy simulation for airfoil stall

  • Dong Li
  • , Yu Qin Jiao
  • , Igor Men'shov
  • , Yoshiaki Nakamura
  • Northwestern Polytechnical University Xian
  • Nagoya University

科研成果: 期刊稿件文章同行评审

9 引用 (Scopus)

摘要

Detached-eddy simulation (DES) is applied to three airfoils with different stall types. The method combines the strong points of Reynolds-averaged Navier-Stokes and large eddy simulation approaches. Spalart-Allmaras model is basically used, which reduces to a RANS formulation near a solid surface and to a subgrid model away from the wall. LU-SGS implicit scheme is employed to solve the model in time. Comparing with the experimental data, it is found that stall angle can be reasonably predicted by the present method.

源语言英语
页(从-至)406-410
页数5
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
26
4
出版状态已出版 - 7月 2005

学术指纹

探究 'Detached-eddy simulation for airfoil stall' 的科研主题。它们共同构成独一无二的学术指纹。

引用此