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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 2008, Vol. 29 ›› Issue (4): 817-822.

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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

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

CLC Number: