航空学报 > 1993, Vol. 14 Issue (1): 1-6

有限空间中激波运动的数值模拟

乐嘉陵, 高铁锁, 曹文祥   

  1. 中国空气动力研究与发展中心,四川 锦阳211信箱 621000
  • 收稿日期:1991-09-02 修回日期:1992-05-08 出版日期:1993-01-25 发布日期:1993-01-25

THE NUMERICAL SIMULATION OF SHOCK WAVE MOTION IN CONFINED SPACE

Le Jia-ling, Gao Tie-suo, Cao Wen-xiang   

  1. China Aerodynamics Research and Development Center, P. O. Box 211, Mianyang,Sichuan. China, 621000
  • Received:1991-09-02 Revised:1992-05-08 Online:1993-01-25 Published:1993-01-25

摘要: 采用一种有限体积的TVD格式模拟喷流产生的启动激波在有限空间内的运动过程。计算获得的激波运动过程与激波在大气中传播时的实验结果一致。在传播过程中出现涡环和多次激波。计算表明,在真空箱为正方体的情况下,激波管出口附近的压力脉冲特性主要取决于有限空间的轴向长度。所得结果对毫秒级激波管喷流模拟装置的真空箱设计有参考价值。

关键词: 激波管, 数值模拟, 激波反射

Abstract: A kind of finite volume TVD Scheme is used to numerically simulate the motion of shock wave projecting into a confined space. The calculated results are in agreement with experimental ones when the shock wave propagates in atmosphere. Following the shock wave, vortex rings and several shock waves appear in the flow field. Calculation indicates that the characteristics of pressure pulses near the open end of the tube depend mainly on the axial length of the confined space of cubic vacuum tank, which is essential for designing the size of vacuum tank of short duration device for simulating exhaust plume at high altitudes.

Key words: shook tubes, numerical simulation, shock wave reflection