论文标题

通过受控的表面粗糙度缓解尖端涡流空化的实验分析

Experimental Analysis of Tip Vortex Cavitation Mitigation By Controlled Surface Roughness

论文作者

Svennberg, Urban, Asnaghi, Abolfazl, Gustafsson, Robert, Bensow, Rickard E.

论文摘要

这项研究提出了实验的结果,在延迟椭圆箔的尖端涡流空化开始时,评估了粗糙度应用。高速视频记录和激光多普勒速度计(LDV)测量可提供有关不同粗糙度模式配置中的空化行为和尖端涡流流属性的更多详细信息。在尖端下游一个和弦长度上,涡旋核区域的角动量测量表明,与光滑的箔条件相比,粗糙度会导致较低的角动量,而在光滑和粗糙的条件下,涡流核心半径保持相似。观察结果表明,与观察到的平滑箔条件相比,在优化的粗糙度模式下,尖端涡流空化开始的空化数量减少了33%,在该条件下,观察到阻力增加约为2%。在测试过程中,没有观察到均匀和不均匀粗糙度分布的气腔创造特性的明显差异。但是,发现阻力较高,具有不均匀的粗糙度分布。

This study presents results of experiments where roughness applications are evaluated in delaying the tip vortex cavitation inception of an elliptical foil. High-speed video recordings and Laser Doppler Velocimetry (LDV) measurements are employed to provide further details on the cavitation behaviour and tip vortex flow properties in different roughness pattern configurations. The angular momentum measurements of the vortex core region at one chord length downstream of the tip indicate that roughness leads to a lower angular momentum compared to the smooth foil condition while the vortex core radius remains similar in the smooth and roughened conditions. The observations show that the cavitation number for tip vortex cavitation inception is reduced by 33 % in the optimized roughness pattern compared to the smooth foil condition where the drag force increase is observed to be around 2 %. During the tests, no obvious differences in the cavitation inception properties of uniform and non-uniform roughness distributions are observed. However, the drag force is found to be higher with a non-uniform roughness distribution.

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