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AEROBREAKUP IN RAREFIED SUPERSONIC GAS FLOWS

机译:稀薄的超音速气体流动的健美交流

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We present new experimental results on the interfacial instabilities and breakup of Newtonian liquid drops suddenly exposed to rarefied, high-speed (Mach 3) air flows. The experimental approach allows for the first time detailed observation of interfacial phenomena and mixing throughout the breakup cycle over a wide range of Weber numbers. Key findings are that Rayleigh-Taylor instability alone is the active mechanism for free stream Weber numbers as low as 28 for low viscosity liquids and that stripping rather than piercing is the asymptotic regime as We→∞ . This and other detailed visual evidence over 26 < We < 2600 are uniquely suitable for testing CFD simulations on the way to basic understanding of aerobreakup over a broad range of conditions.
机译:我们展示了纽托利液滴的界面不稳定性和分解的新实验结果突然暴露于稀薄,高速(马赫3)空气流动。实验方法允许首次详细观察界面现象并在整个韦伯号上整个分手循环混合。关键发现是单独的瑞利 - 泰勒不稳定性是游离流量的有效机制,对于低粘度液体,剥离而不是穿孔是渐近的制度,就像我们→〗一样。超过26 <我们<2600的其他具体视觉证据是独特的,适用于在广泛的条件下对Aerobreakup的基本理解的基本理解的方式测试CFD模拟。

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