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Insight into tip vortex cavitation using velocity field measurements

机译:使用速度场测量洞察尖端涡旋空化

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Statistics of tip vortex core pressure are estimated from instantaneous Stereo PIV measurements of the velocity field. The tip vortex was generated by a rectangular planform (aspect ratio 2), elliptically-loaded fin with a NACA66 foil shape. A set of 500 velocity field realizations were acquired at each of three angles of attack. Estimates of pressure for each measured velocity field were computed using a finite-element scheme that minimized error propagation from the measured velocity field. Histograms of core pressure show that the mean core pressure followed expected scaling with vortex strength, and that the width of the distribution is inversely proportional to vortex strength.
机译:尖端涡旋芯压的统计数据从速度场的瞬时立体声PIV测量估计。尖端涡旋由矩形扁平型(纵横比2),椭圆形翅片具有Naca66箔形状产生。在三个攻击角度中获得了一组500速度场的实现。使用有限元方案计算每个测量速度场的压力估计,该有限元方案可最小化从测量的速度场从误差传播。核心压力的直方图表明,平均芯压力遵循预期的涡流缩放,并且分布的宽度与涡流强度成反比。

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