CHINESE JOURNAL OF COMPUTATIONAL PHYSICS ›› 2006, Vol. 23 ›› Issue (3): 361-365.

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Numerical Investigation of Complex 3-D Supersonic Flows with a Self-Adaptive Tree Mesh

TIAN Zheng-yu, LI Hua, PAN Sha   

  1. Institute of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, China
  • Received:2005-01-17 Revised:2005-06-24 Online:2006-05-25 Published:2006-05-25

Abstract: Based on an initial structural mesh, a data structure for a 3-D body-fitted tree mesh was built. Simplified algorithms were developed for anisotropic self-adaptive split and mergence. In order to reduce the number of mesh cells we set restrictive self-adaptive levels for different zones divided in advance. A method of protective mesh split for structures in flow field was developed. Numerical simulations with different complex supersonic flow patterns were shown. It is proved that the anisotropic self-adaptive tree mesh is effective with less mesh cells and convenient for mesh refinement. High resolution for Now field is obtained.

Key words: self-adaptation, tree mesh, anisotropy, 3-D shock/shock interaction

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