Relating Trailing Vortex Cavitation Inception To Single Phase Flow Measurements

S. Green, A. Acosta
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引用次数: 0

Abstract

The single phase and cavitating tip vortex shed by a NACA .66-209 rounded tip hydrofoil has been studied. Single phase measurements of instantaneous flow velocity were made by taking double pulsed holograms of microbubbles moving in and around the vortex core. The tailored air bubble technique of Ooi and Acosta (1983) was employed to measure both the mean and fluctuating single phase vortex core static pressure. Cavitation inception was determined visually. The flow in the vortex core is highly unsteady. The r.m.s. axial velocity fluctuation can be as high as 0.2Uoo Core pressure fluctuations greater than the freestream dynamic pressure have been measured. These fluctuations are thought to accompany local axial velocity fluctuations. With saturated water, inception occurs at mean core pressures above the vapour pressure. However, the pressure fluctuations are certainly substantial enough to account for these elevated inception indices. The fluctuations also explain why inception occurs immediately downstream of the hydrofoil. The rapid establishment of fully developed trailing vortex cavitation when the cavitation number is reduced below inception is attributable to the small variation in mean core pressure with downstream distance. The inception index decreases dramatically with decreasing dissolved air content. The cause of this decrease is not known.
尾涡空化起始与单相流测量的关系
研究了NACA .66-209型圆尖水翼的单相空化尖涡脱落。通过拍摄微气泡在涡旋中心内和周围运动的双脉冲全息图,实现了瞬时流速的单相测量。采用Ooi和Acosta(1983)的定制气泡技术测量平均和波动单相涡芯静压。通过目测确定空化起始。涡旋核心内的流动是非稳定的。轴向速度波动可高达0.2 μ m,岩心压力波动大于自由流动压。这些波动被认为伴随着局部轴向速度波动。对于饱和水,起始发生在高于蒸汽压力的平均堆芯压力下。然而,压力波动肯定是巨大的,足以解释这些高启动指数。这种波动也解释了为什么初始阶段发生在水翼的下游。当空化数减少到起始数以下时,尾涡空化充分发育的迅速建立是由于平均岩心压力随下游距离的变化较小。随着溶解空气含量的降低,初始指数显著降低。这种减少的原因尚不清楚。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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