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Volume 25 Issue 6
Jun.  1999
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Journal of Beijing University of Aeronautics and Astronautics  > 1999  >  25(6): 680-683.
Cai Guobiao, Zhuang Fenggan. Direct Numerical Simulation on 2-D H2/O2 Mixture and Flow[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(6): 680-683. (in Chinese)
Citation: Cai Guobiao, Zhuang Fenggan. Direct Numerical Simulation on 2-D H2/O2 Mixture and Flow[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(6): 680-683. (in Chinese)
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Direct Numerical Simulation on 2-D H2/O2 Mixture and Flow

  • 1.

    Beijing University of Aeronautics and Astronautics, School of Astronautics

  • 2. Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 31 May 1999
  • Publish Date: 30 Jun 1999
    Abstract
  • The present work uses high order accuracy compact difference scheme and composites the computer code for 2-dimensional compressible low velocity H2/O2 mixing flow evaluating with time growth. Computation for subsonic, transonic and supersonic H2/O2 mixing flow with Reynolds number being 400 and Mach number being 0.4 (upper part H2) and 1.57 (bottom part O2) has been done and obtained computation results. The computation results are analyzed and studied.

     

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    • References(1)
  • 1. 蔡国飙,张化照,庄逢甘.氢氧发动机推力室化学反应流场计算.北京航空航天大学学报,1998,24(6):671~675 2. Fu D X, Ma Y W. A high order accurate difference scheme for complex flow fields. Journal of Computational Physics, 1997,134:1~15 3. Michalke A. On the inviscid instability of the hyperbolic-tangent velocity profile. Journal of Fluid Mechanics, 1964, 19:543~556
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