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Numerical and experimental analysis of cavitation inception behaviour for high-skewed low-noise propellers

机译:高偏斜低噪声螺旋桨空化初始行为的数值和实验分析

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Numerical and experimental investigations of two highly skewed low-noise propellers with a slight alteration in the tip geometry are conducted in both wetted and cavitating flows. The performance of the propellers is measured in open water and inclined setups at different operating conditions and high speed video recordings are used to determine tip vortex cavitation inception behaviour. The numerical simulations are conducted by employing the Implicit Large Eddy Simulation on appropriate grid resolutions for tip vortex propagation, at least 32 cells per vortex diameter according to our previous studies. In order to investigate cavitation inception characteristics of the propellers, different inception prediction methods are employed and evaluated at different advance ratios.It is shown that in addition to the well-captured difference in e.g. the amount of cavitation, the simulations are capable of correctly predicting the small but crucial differences in flow features and cavitation inception characteristics of the two propeller designs. Numerical predictions of the cavitation inception charts are also compared successfully with the measured data where three different types of cavitation patterns are investigated in details. Supported by the experimental videos, the interaction between the tip vortex and trailing vortices and their impact on the pressure field and the cavitation inception are analyzed. It is shown that the numerical simulation can provide further details about the vortical flow structures, and their contributions to cavitation, and is a powerful tool in advanced propeller design stages.
机译:两个高度倾斜低噪声螺旋桨的数值和实验研究,尖端几何形状略微改变,在湿润和空化流动中进行。螺旋桨的性能在开放水中测量,在不同的操作条件下,高速视频录制用于确定尖端涡旋空化截头行为。通过在适当的网格分辨率上采用隐式的大涡模拟来进行数值模拟,以进行尖端涡旋传播,根据我们以前的研究,每涡流直径至少为32个细胞。为了研究螺旋桨的空化初始特性,在不同的预先比率下采用和评估不同的初始预测方法。如图所示,除了占用良好捕获的差异之外。空化量,模拟能够正确地预测两种螺旋桨设计的流动特征和空化初始特性的小但重要的差异。还使用测量数据比较空化初始图表的数值预测,其中详细地研究了三种不同类型的空化图案。通过实验视频支持,分析了尖端涡旋和落叶之间的相互作用及其对压力场的影响以及空化初始化。结果表明,数值模拟可以提供有关涡流结构的进一步细节,以及它们对空化的贡献,并且是高级推进器设计阶段的强大工具。

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