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二维凹面腔内暂冲式激波聚焦机理的实验

王川 陈鑫 荣康 赵罡 谭胜

王川, 陈鑫, 荣康, 赵罡, 谭胜. 二维凹面腔内暂冲式激波聚焦机理的实验[J]. 航空动力学报, 2018, 33(9): 2112-2122. doi: 10.13224/j.cnki.jasp.2018.09.008
引用本文: 王川, 陈鑫, 荣康, 赵罡, 谭胜. 二维凹面腔内暂冲式激波聚焦机理的实验[J]. 航空动力学报, 2018, 33(9): 2112-2122. doi: 10.13224/j.cnki.jasp.2018.09.008
Experiment of transient shock wave focusing performance in two-dimensional concave cavity[J]. Journal of Aerospace Power, 2018, 33(9): 2112-2122. doi: 10.13224/j.cnki.jasp.2018.09.008
Citation: Experiment of transient shock wave focusing performance in two-dimensional concave cavity[J]. Journal of Aerospace Power, 2018, 33(9): 2112-2122. doi: 10.13224/j.cnki.jasp.2018.09.008

二维凹面腔内暂冲式激波聚焦机理的实验

doi: 10.13224/j.cnki.jasp.2018.09.008
基金项目: 国家自然科学基金青年科学基金(51106178)

Experiment of transient shock wave focusing performance in two-dimensional concave cavity

  • 摘要: 针对两级脉冲爆震发动机中第二级凹面腔内激波聚焦起爆能量和周期的研究,设计了二维凹面腔内暂冲式激波聚焦实验系统。通过分析粒子图像测速系统捕捉的照片和动态压力数据,获得了凹面腔内激波聚焦高压区压力特性和多循环流场演化特征。并且开展了A和B两种型面凹面腔的对比实验,进一步分析了多循环激波聚焦的形成机理。结果表明:入射激波第一次在凹面腔底部聚焦后形成的聚焦反射激波在喷口射流边界上发生反射,产生的反射激波再次在凹面腔底部聚焦,形成了第二次激波聚焦,如此往复便形成了周期性的激波聚焦,聚焦频率高达7~10kHz;并且,速度场和射流强度随入射激波碰撞而减弱,在排气过程中又增强,呈现周期性变化。

     

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出版历程
  • 收稿日期:  2017-04-25
  • 刊出日期:  2018-09-28

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