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CAVITATION INCEPTION BEHIND A JET-PROPELLED BODY

机译:喷气机推进的身体背后的空化初始化

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Cavitation inception behind an axisymmetric body driven by a waterjet has been studied experimentally and numerically. Water tunnel tests have been performed with the body mounted on a force balance. The transom of the body contained a nozzle located along the centerline. Tests were carried out for various water tunnel speeds such that jet velocity ratio, V{sub}J/U, could be varied in the range 0 to 2. Distinctly different cavitation patterns were observed at zero jet velocity (when cavitation appeared in spiral vortices in such flows) and at a various jet velocity ratios (when cavitation appeared between counter-rotating vortices around the jet in such flows). Cavitation inception/disappearance has been determined visually. The body drag was also measured. An analytical method for determination of cavitation inception index has been developed on the basis of a viscous-inviscid interaction concept, with employment of special semi-empirical approximations for vortices and consideration of surface tension. These approximations have been preliminarily validated for nozzle jet cavitation (for nozzle discharge in coflow). It was assumed that visualization allows detection of cavities (bubbles) of 0.4 mm-0.5 mm diameter or larger. The cavitation inception index is defined as the cavitation index for cavities of such minimum diameter when these cavities are located between counter-rotating vortices. The initial comparison of predicted and measured values of the cavitation inception index shows good agreement.
机译:通过实验和数值研究了水射流驱动的轴对称体背后的空化初始化。已经使用了部队平衡的主体进行了水隧道试验。身体的横向包含沿着中心线的喷嘴。对各种水隧道速度进行测试,使得喷射速度比V {Sub} J / U可以在0到2的范围内变化。在零喷射速度下观察到明显不同的空化图案(当空化出现在螺旋涡流时在这种流动中,并且在各种喷射速度比(当空化时出现在这种流动的射流周围的反向旋转涡旋之间)。在视觉上确定了空化初始/消失。还测量了身体阻力。基于粘性反相互作用概念开发了一种用于测定空化初始指标的分析方法,采用了用于涡流的特殊半经验近似和表面张力的考虑。已经预先验证了用于喷嘴喷射空化(用于在CoFlow中的喷嘴放电)预先验证这些近似值。假设可视化允许检测0.4mm-0.5mm直径或更大的腔体(气泡)。空化初始指数被定义为当这些空腔位于反向旋转涡流之间时,该空化初始指数被定义为这种最小直径的空腔。空化初始指数的预测和测量值的初始比较显示了良好的一致性。

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