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Experimental study on a heavy-gas cylinder accelerated by cylindrical converging shock waves

机译:圆柱会聚冲击波加速重汽缸的实验研究

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The Richtmyer-Meshkov instability behavior of a heavy-gas (SF_6) cylinder accelerated by a cylindrical converging shock wave is studied experimentally. A curved wall profile is well-designed based on the shock dynamics theory [Phys. Fluids, 22: 041701 (2010)] with an incident planar shock Mach number of 1.2 and a converging angle of 15° in a 95mm× 95 mm square cross-section shock tube. The SF_6 cylinder mixed with the glycol droplets flows vertically through the test section and is illuminated horizontally by a laser sheet. The images obtained only one per run by an ICCD (intensified charge coupled device) combined with a pulsed Nd:YAG laser are first presented and the complete evolution process of the SF_6 cylinder is then captured in a single test shot by a high-speed video camera combined with a high-power continuous laser. In this way, both the developments of the first counter-rotating vortex pair and the second counter-rotating vortex pair with an opposite rotating direction from the first one are observed. The experimental results indicate that the phenomena induced by the converging shock wave and the reflected shock formed from the center of convergence are distinct from those found in the planar shock case.
机译:实验研究了圆柱形会聚冲击波加速的重气(SF_6)气缸的Richtmyer-Meshkov不稳定性行为。弯曲壁轮廓是根据冲击动力学理论精心设计的。流体,22:041701(2010)],在95mm×95 mm方形截面的冲击管中,入射平面冲击马赫数为1.2,会聚角为15°。混合有乙二醇滴的SF_6圆柱体垂直流过测试部分,并被激光片水平照射。首先介绍了由ICCD(增强电荷耦合器件)结合脉冲Nd:YAG激光器每次运行仅获得的图像,然后通过高速视频在一次测试中捕获了SF_6圆柱体的完整演变过程。摄像头与大功率连续激光结合。以这种方式,观察到第一反向旋转涡流对和第二反向旋转涡流对具有与第一反向旋转涡流相反的方向。实验结果表明,由会聚冲击波引起的现象和由会聚中心形成的反射冲击与在平面冲击情况下发现的现象不同。

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