The aeroelastic characteristics of high aspect ratio wing

Fan Yang, Zhufeng Yue, Lei Li

科研成果: 期刊稿件文章同行评审

3 引用 (Scopus)

摘要

Owing to the elasticity, the large deformation was brought in the high aspect ratio wing in the flight. The large deformation had a great influence on the flight performance. In this paper, the loosely coupled method was used for the research of high aspect ratio wing aeroelastic problems. The Navier-Stokes equations were solved for fluid domain computation, and the nonlinear finite element method was adopted for solid domain computation. The data exchange program and mesh regeneration progress were adopted for fluid-structure interface problem. Finally, the aerodynamic characteristics of high aspect ratio wing were obtained under different fly conditions. In addition, to validate the proposed method, the flutter analysis of AGARD 445.6 wing is carried out and compared with the experimental data. The numerical result validates the proposed computational fluid dynamics/computational structural mechanics method.

源语言英语
页(从-至)2543-2556
页数14
期刊Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering
230
14
DOI
出版状态已出版 - 1 12月 2016

指纹

探究 'The aeroelastic characteristics of high aspect ratio wing' 的科研主题。它们共同构成独一无二的指纹。

引用此