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arXiv 2304.01477physics.flu-dyn
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关于液滴下落速度

On droplet falling velocity

Wenjie Ji, Siyuan Wang, Jiguang Hao, J. M. Floryan

AI总结:

本研究通过高速摄影实验发现液滴撞击前未达终端速度,提出并验证了一种考虑空气动阻力的动力学模型,可准确预测液滴下落速度。

摘要:

利用高速摄影技术研究了撞击研究中使用的液滴速度。研究确定液滴在典型撞击前未达到终端速度,这引发了如何预测撞击速度的问题。通过实验对这一问题进行了研究,并利用结果验证了理论模型。实验使用了直径0.70mm至4.0mm的液滴,密度为791kg/m3至1261.5kg/m3的液体,粘度为1.0mPa s至1390.0mPa s,释放高度最高达1.0m。环境压力在大气压和25kPa之间变化。结果表明,液滴速度随液滴直径、液体密度、释放高度的增加以及环境压力的降低而增加,但随粘度变化很小。提出了一种考虑空气动阻力的简单动力学模型。该模型使用经验公式确定瞬时阻力系数,预测的速度与本研究参数范围内的实验数据吻合良好。它为液滴撞击研究的设计提供了有价值的工具。

英文摘要:

Droplet velocities used in impact studies were investigated using high-speed photography. It was determined that droplets do not reach terminal velocity before a typical impact, raising the question of how to predict impact velocity. This question was investigated experimentally, and the results were used to validate a theoretical model. Experiments used droplets with diameters 0.70mm to 4.0mm, liquids with a density of 791kg/m3 to 1261.5kg/m3, and viscosities 1.0mPa s to 1390.0mPa s, release height up to 1.0m. The ambient pressure was varied between atmospheric and 25kPa. It was shown that the droplet velocity increased with the droplet diameter, liquid density, release height, and ambient pressure reduction but changed marginally with viscosity. A simple dynamic model accounting for the aerodynamic drag was proposed. This model, which uses empirical formulae to determine the instantaneous drag coefficient, predicts velocity, which agrees well with the experimental data within the range of parameters used in this study. It provides a valuable tool for the design of droplet impact studies.

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