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ACTA AERONAUTICAET ASTRONAUTICA SINICA ›› 1996, Vol. 17 ›› Issue (S1): 68-71.

• 论文 • Previous Articles     Next Articles

THE SCHEME EFFECTS OF NUMERICAL SOLUTIONS FOR SHOCK/BOUNDARY LAYER INTERACTION

Yan Chao, Chen Liang   

  1. Institute of Fluid Dynamics, Beijing University of Aeronautics and Astronautics, Beijing, 100083
  • Received:1996-01-25 Revised:1996-04-19 Online:1996-11-25 Published:1996-11-25

Abstract: Shock/boundary layer interaction is simulated by solving 2 dimensional N S equations using different numerical schemes, including Roe's FDS scheme and van Leer's FVS scheme fitted with different limiters. The computed flow phenomenon is analyzed and a study on the varying scheme effects is made.Some new opinion is presented.

Key words: shock boundary/layer interaction, numerical solutions, resolution

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