CHINESE JOURNAL OF COMPUTATIONAL PHYSICS ›› 1997, Vol. 14 ›› Issue (S1): 496-498.

Previous Articles     Next Articles

NUMERICAL STUDY OF WAVE STRUCTURE OF ROCKET JET FLOW

Yang Hongwei, Ma Dawei, Zhang Fuxiang   

  1. Faculty 102, University of Science and Technology, Nanjing 210094
  • Received:1997-01-16 Revised:1997-05-04 Online:1997-12-25 Published:1997-12-25

Abstract: According to the MUSCL scheme with some modifications, the flow field structure of jet is numerically simulated. The results show that the present scheme has high resolution of shock wave, nonoscillation and high efficiency.

Key words: rocket jet flow, numerical simulation, shock wave

CLC Number: