航空学报 > 2008, Vol. 29 Issue (4): 817-822

一种新的动网格方法及其应用

刘学强1,李青2,柴建忠2,N.Qin3   

  1. 1南京航空航天大学 空气动力学系 2第一飞机设计研究院 3 Sheffield University
  • 收稿日期:2007-05-22 修回日期:2008-01-19 出版日期:2008-07-10 发布日期:2008-07-10
  • 通讯作者: 刘学强1

A New Dynamic Grid Algrithm and Its Application

Liu Xueqiang1, Li Qing2, Chai Jianzhong2, N. Qin3   

  1. 1 Department of Aerodynamics, Nanjing University of Aeronantics and Astronautics 2 The First Aircraft Institute of AVICI 3 Sheffield University
  • Received:2007-05-22 Revised:2008-01-19 Online:2008-07-10 Published:2008-07-10
  • Contact: Liu Xueqiang1

摘要:

介绍了一种新型的动网格方法。该方法以Delauney图为基础进行整个网格的移动变形:首先是生成满足Delauney特性的Delauney图;然后把对网格移动的特性映射到Delauney图的移动上;最后把网格点在Delauney图以映射的方式进行重新定位而得到新的网格点坐标,从而得到移动后的网格。该方法不需要迭代,因而效率高,并且能适用于任意拓扑结构的网格。以翼身组合体的机翼颤振、翼身融合体的变体过程的非定常流动等为例来说明该方法的高效性及适用面广等特点。

关键词: 动网格, 非定常流动, 计算流体力学, 飞翼, Delauney图

Abstract:

A new dynamic grid algorithm is proposed in this article. It is based on a Delauney map, out of which deformation is carried out. Firstly, the Delauney map is generated; secondly, the mapping coefficients are calculated and the deformation is done on the Delauney map; finally, the grid points are relocated on the deformed Delauney map, and the final dynamic grid is obtained. This dynamic algorithm is noniterative, therefore it is highly efficient and it also offers cell topological flexibility. Several unsteady cases are computated to demonstrate its roboustness, including a deformed wingbody combination and the unsteady flows during the deforming of the body of the flyingwing.

Key words: dynamic , grid,  , unsteady , flow,  , computational , fluid , dynamics,  , flying , wing,  , Delauney , map

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