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首页> 外文期刊>Journal of Fluid Mechanics >Role of 'splashing' in the collapse of a laser-generated cavity near a rigid boundary
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Role of 'splashing' in the collapse of a laser-generated cavity near a rigid boundary

机译:“飞溅”在刚性边界附近激光产生的腔体坍塌中的作用

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Vapour cavities in liquid flows have long been associated with cavitation damage to nearby solid surfaces and it is thought that the final stage of collapse, when a high-speed liquid jet threads the cavity, plays a vital role in this process. The present study investigates this aspect of the motion of laser-generated cavities in a quiescent liquid when the distance (or stand-off) of the point of inception from a rigid boundary is between 0.8 and 1.2 times the maximum radius of the cavity. Numerical simulations using a boundary integral method with an incompressible liquid impact model provide a frame work for the interpretation of the experimental results. It is observed that, within the given interval of the stand-off parameter, the peak pressures measured on the boundary at the first collapse of a cavity attain a local minimum, while at the same time there is an increase in the duration of the pressure pulse. This contrasts with a monotonic increase in the peak pressures as the stand-off is reduced, when the cavity inception point is outside the stated interval. This phenomenon is shown to be due to a splash effect which follows the impact of the liquid jet. Three cases are chosen to typify the splash interaction with the free surface of the collapsing cavity: (i) surface reconnection around the liquid jet; (ii) splash impact at the base of the liquid jet; (iii) thin film splash. Hydrodynamic pressures generated following splash impact are found to be much greater than those produced by the jet impact. The combination of splash impact and the emission of shock waves, together with the subsequent re-expansion, drives the flow around the toroidal cavity producing a distinctive double pressure peak.
机译:长期以来,液体流动中的蒸气腔与空化损坏附近的固体表面有关,人们认为,当高速液体射流穿过腔时,崩溃的最后阶段在该过程中起着至关重要的作用。当静止点的起始点与刚性边界的距离(或间距)在空腔最大半径的0.8到1.2倍之间时,本研究研究了静态液体中激光生成空腔运动的这一方面。使用边界积分法和不可压缩的液体冲击模型进行数值模拟,为解释实验结果提供了框架。可以观察到,在给定的间隔参数间隔内,在腔体第一次塌陷时在边界处测得的峰值压力达到局部最小值,而同时压力持续时间增加了。脉冲。当腔体的起始点在规定的间隔之外时,这与峰值压力的单调增加形成了鲜明的对比,因为峰值减小了,所以这种间隔减小了。示出该现象是由于在液体射流的冲击之后的飞溅效应。选择三种情况来代表与塌陷腔的自由表面的飞溅相互作用:(i)围绕液体射流的表面重新连接; (ii)液体喷射器底部的飞溅冲击; (iii)薄膜飞溅。发现飞溅冲击之后产生的流体动力压力要比喷射冲击产生的流体动力压力大得多。飞溅冲击和冲击波发射的结合,以及随后的重新膨胀,驱使环形腔周围的气流产生独特的双压力峰值。

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