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Numerical study of cavitation inception in the near field of an axisymmetric jet at high Reynolds number

机译:高雷诺数轴对称射流近场空化开始的数值研究

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摘要

Cavitation inception in the near field of high Reynolds number axisymmetric jets is analyzed using a simplified computational model. The model combines a vorticity-stream-function finite-difference scheme for the simulation of the unsteady flow field with a simplified representation for microscopic bubbles that are injected at the jet inlet. The motion of the bubbles is tracked in a Lagrangian reference frame by integrating a semiempirical dynamical equation which accounts for pressure, drag, and lift forces. The likelihood of cavitation inception is estimated based on the distributions of pressure and microscopic bubbles. The computations are used to examine the role of jet slenderness ratio, Reynolds number, bubble size, and bubble injection location on the cavitation inception indices. The results indicate that, for all bubble sizes considered, the cavitation inception index increases as the jet slenderness ratio decreases. Larger bubbles entrain more rapidly into the cores of concentrated vortices than smaller bubbles, and the corresponding inception indices are generally higher than those of smaller bubbles. The inception indices for larger bubbles are insensitive to the injection location, while the inception indices of smaller bubbles tend to increase when they are injected inside the shear layer near the nozzle lip. Although it affects the bubble distributions, variation of the Reynolds number leads to insignificant changes in pressure minima and in the inception indices of larger bubbles, having noticeable effect only on the inception indices of smaller bubbles. Computed results are consistent with, and provide plausible explanations for, several trends observed in recent jet cavitation experiments. (C) 2000 American Institute of Physics. [S1070-6631(00)00310-X]. [References: 30]
机译:使用简化的计算模型分析了高雷诺数轴对称射流近场中的气穴现象。该模型将用于模拟非恒定流场的涡流函数有限差分方案与在喷射口注入的微小气泡的简化表示结合在一起。气泡的运动在Lagrangian参考系中通过集成半经验动力学方程来跟踪,该方程考虑了压力,阻力和升力。基于压力和微小气泡的分布来估计气蚀开始的可能性。该计算用于检查射流细长比,雷诺数,气泡大小和气泡注入位置对空化开始指数的作用。结果表明,对于所考虑的所有气泡尺寸,当喷射细长比降低时,气蚀起始指数会增加。与较小的气泡相比,较大的气泡比较小的气泡更快速地夹带进入涡旋的核心,并且相应的起始指数通常高于较小的气泡。较大气泡的起始指数对注入位置不敏感,而较小气泡的起始指数在将其注入喷嘴唇附近的剪切层内时往往会增加。尽管它影响气泡分布,但雷诺数的变化会导致最小压力和较大气泡起始指数的变化不明显,仅对较小气泡起始指数有显着影响。计算结果与最近喷气空化实验中观察到的几种趋势一致,并提供了合理的解释。 (C)2000美国物理研究所。 [S1070-6631(00)00310-X]。 [参考:30]

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