航空学报 > 2000, Vol. 21 Issue (3): 193-195

被动式引射器内两相流数值模拟

杨涓, 何洪庆, 毛根旺   

  1. 西北工业大学航天工程学院 陕西西安 710072
  • 收稿日期:1999-02-22 修回日期:1999-05-16 出版日期:2000-06-25 发布日期:2000-06-25

NUMERICAL SIMULATION OF TWO PHASE FLOW WITHIN PASSIVE EJECTORS

YANG Juan,HE Hong-qing,MAO Gen-wang   

  1. College of Astronautics, Northwesten Polytechnic University, Xi'an 710072, China
  • Received:1999-02-22 Revised:1999-05-16 Online:2000-06-25 Published:2000-06-25

摘要: 把气相二维欧拉方程的隐式矢通量分裂近似因子分解法与固相粒子的特征线解法进行耦合,对被动式引射器内两相流场进行数值模拟,确定产生激波的喷管出口压强,分析不同引射器结构对引射效果的影响,并获得了一种最佳结构。研究结果可以为被动式引射器的设计与使用提供依据。

关键词: 矢通量分裂, 因子分解, 引射器, 两相流, 特征线

Abstract: The two phase flow within a passive ejector was simulated by employing the method of implicit vector flux splitting scheme combined with the approximate factorization algorithm for 2 D Euler equations, coupled with the characteristic method of the particle phase. The minimum outlet pressure of the nozzle was found when the normal shock wave was presented down stream within the ejector, and the effects of different ejector structures on the position of shock wave were analyzed. From this, the optimum structure was obtained. The calculated results provide the basis for the designing and using of passive ejectors.

Key words: vecto r flux sp lit t ing scheme, app roximate facto rizat ion algo rithm, ejecto r, two-phase flow, characterist ic method

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