二维凹面腔内暂冲式激波聚焦机理的实验  

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

作　　者：王川 陈鑫[1,2] 荣康 赵罡[4] 谭胜[1] WANG Chuan;CHEN Xin;RONG Kang;ZHAO Gang;TAN Sheng(Aeronautics and Astronautics Engineering College,Air Force Engineering University,Xi＇an 710038,China;Collaborative Innovation Center for Advanced Aero-Engine,Beijing 100191,China;Unit 94710,the Chinese People＇s Liberation Army,Wuxi Jiangsu 214142,China;Training Department,Air Force Engineering University,Xi＇an 710038,China)

机构地区：[1]空军工程大学航空航天工程学院,西安710038 [2]先进航空发动机协同创新中心,北京100191 [3]中国人民解放军94710部队,江苏无锡214142 [4]空军工程大学训练部,西安710038

出　　处：《航空动力学报》2018年第9期2112-2122,共11页Journal of Aerospace Power

基　　金：国家自然科学基金青年科学基金(51106178)

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。Two-dimensional transient shock wave focusing experiment system was designed to investigate the shock wave focusing initiation energy of two-stage pulse detonation engine.Dynamic pressure sensors and particle image velocimetry system were adopted to capture the dynamic pressure of the cavity bottom vertex and the velocity vector field during multi-cycle of shock focus.Furthermore,the cavities of type A and B were used in contrast tests and the velocity vector field was analyed in the meantime.It was found that the first focus was caused by incident shock produced by diaphragm rupture.The post-focus reflected wave formed immediately after shock focus reflected at jet boundary of the nozzle exit and generated the re-reflected wave.The re-reflected wave acted a incident shock in the secondcycle and contributed to the second shock focus,then periodic shock focus formed.The focus frequency was up to 7-10 kHz.In addition,the velocity field and the strength of the jet weakened with the collision of incident shock waves,then enhanced when high-pressure flow was exhausted,forming a cyclical change.

关 键 词：二维凹面腔 激波聚焦 粒子图像测速系统 多循环流场 压力特性 聚焦频率 

分 类 号：V231.22[航空宇航科学与技术—航空宇航推进理论与工程]