CHINESE JOURNAL OF COMPUTATIONAL PHYSICS ›› 1997, Vol. 14 ›› Issue (S1): 528-529,531.

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A STUDY OF SIMPLIFIED FLUX-VECTOR SPLITTING ALGORITHM

Ma Handong1, Wu Liyi1, Li Suxun2   

  1. 1. Beijing University of Aeronautics and Astronautics, 100083;
    2. Beijing Institute of Aerodynamics, 100074
  • Received:1996-10-21 Revised:1997-05-19 Online:1997-12-25 Published:1997-12-25

Abstract: A hybird scheme is constructed by Steger-Warming Splitting and its modified algorithm.The enlargment factor of pressure difference is used to prompt ability of flow field resolution.Meanwhile,a special matrix splitting method is adopted and makes matrices very easy to compute.Three examples of two-dimensional fluid flows containing shocks and/or boundary layer demonstrate the efficiency and accuracy of this new scheme.

Key words: flux-vector splitting, supersonic flow, numerical simulation

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