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激波绕射触发爆震波的试验研究
引用本文:韩启祥,戈雯,王家骅.激波绕射触发爆震波的试验研究[J].航空动力学报,2007,22(11):1803-1807.
作者姓名:韩启祥  戈雯  王家骅
作者单位:南京航空航天大学,能源与动力学院,南京,210016
摘    要:在单爆震试验平台上对激波绕射触发爆震波的特性进行了试验研究.针对不同的激波反射器结构尺寸,测量了爆震管内气体压力变化历程及火焰传播速度,获得了不同工况下激波绕射触发爆震波的特性.结果表明:激波反射器对爆震波的形成有促进作用,并取决于反射器中的反射锥及反射孔板的结构与尺寸;在反射锥堵塞比一定的情况下,存在最佳反射锥锥角使得爆震波的形成距离最小;而反射锥与反射孔板的间距增大,爆震波形成距离增大,一旦形成稳定的爆震波后,反射器对爆震波压力的影响不大.

关 键 词:航空、航天推进系统  激波  绕射  爆震波  DDT距离  压力  波绕射  触发  爆震波  试验  研究  shock  diffraction  initiation  detonation  影响  波压力  稳定  波形  间距  最小  距离  锥角  最佳  存在  情况  堵塞比
文章编号:1000-8055(2007)11-1803-05
收稿时间:2007/4/24 0:00:00
修稿时间:2007年4月24日

Investigation on the detonation initiation by shock diffraction
HAN Qi-xiang,GE Wen and WANG Jia-hua.Investigation on the detonation initiation by shock diffraction[J].Journal of Aerospace Power,2007,22(11):1803-1807.
Authors:HAN Qi-xiang  GE Wen and WANG Jia-hua
Institution:College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
Abstract:This paper reports on the investigation of detonation initiation by shock diffraction on a set of the single detonation.With kinds of different reflector,the pressure histories and flame propagation velocities in the detonator tube were measured to study the characteristics of detonation initiation.The results indicate that the shock diffraction could prompt the initiation of detonation,and which were affected by the dimension of the cone and plate of reflector.With same blockage ratio of the cone,there has a optimal cone angle where the DDT(deflagration to detonation transition) distance was minimum.The DDT distance would be lengthened when the gap between the cone and plate was increased,but the pressure of detonation wave was influenced little by the reflector.
Keywords:aerospace propulsion system  shock wave  diffraction  detonation  deflagration to detonation transition(DDT) distance  pressure
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