Euler solution of a 3D wing-body configuration with aileron

被引：0
|
作者：
Li, J. [1 ]
Zhu, Z.Q. [1 ]
Wu, Z.C. [1 ]
Chen, Z.M. [1 ]
机构：
[1] Sch. of Sci., Beijing Univ. of Aerona. and Astron., Beijing 100083, China
来源：
| 2000年 / Beijing University of Aeronautics and Astronautics (BUAA)卷 / 26期
关键词：
Computational fluid dynamics - Flow of fluids - Numerical analysis - Three dimensional;
D O I：
暂无
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学科分类号：
摘要：
Euler method for solving the flow around a wing-body configuration with deflection of control surface (aileron) is presented. Using the combination of patched grid and domain decomposition techniques, the complex flow around this kind of configuration is effectively solved. An internal coupling condition is given to make the conservation of flux satisfied. In the computation Van Leer's scheme is used to discretize the inviscid flux terms and a new Limiter function is constructed to realize TVD character. Numerical results show that the present method is an effective one for solving the flow around wing-body configuration with control surface deflection.
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