Jiang Shuaishuai, Cai Wei, Xie Jin, He Dong, Wang He, Si Ting, Luo Xisheng
Advanced Propulsion Laboratory, Department of Modern Mechanics, University of Science and Technology of China, Hefei 230026, China.
State Key Laboratory of High-Temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190, China.
Rev Sci Instrum. 2024 Aug 1;95(8). doi: 10.1063/5.0217768.
A shock-tube facility capable of generating a planar shock with the Mach number higher than 3.0 is developed for studying Richtmyer-Meshkov instability induced by a strong shock wave (referred to as strong-shock RMI). Shock enhancement is realized through the convergence of shock within a channel with the profile determined by using shock dynamics theory. The facility is designed considering the repeatability of shock generation, transition of shock profile, and effects of viscosity and flow choking. By measuring the dynamic pressure of the tube flow using pressure sensors and capturing the shock movement through the high-speed shadowing technique, the reliability and repeatability of the shock tube for generating a strong planar shock are first verified. Particular emphasis is then placed on the ability of the facility to study strong-shock RMI, for which a thin polyester film is adopted to form the initial interface separating gases of different densities. The results indicate that the shock tube is reliable for conducting strong-shock RMI experiments.
为了研究由强冲击波引发的瑞利-泰勒-麦什科夫不稳定性(简称为强冲击RMI),开发了一种能够产生马赫数高于3.0的平面冲击波的激波管装置。通过利用激波动力学理论确定通道轮廓,使激波在通道内汇聚,从而实现激波增强。该装置在设计时考虑了激波产生的可重复性、激波轮廓的转变以及粘性和流动阻塞的影响。通过使用压力传感器测量管内流动的动态压力,并通过高速阴影技术捕捉激波运动,首先验证了激波管产生强平面冲击波的可靠性和可重复性。然后特别强调了该装置研究强冲击RMI的能力,为此采用了一层薄聚酯薄膜来形成分隔不同密度气体的初始界面。结果表明,该激波管对于进行强冲击RMI实验是可靠的。