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Wind tunnel study of separated and reattaching flows by particle image velocimetry and pressure measurements

机译:通过粒子图像测速和压力测量研究分离和再附着流的风洞

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摘要

This article presents a comprehensive investigation on the separated and reattaching flows over a blunt flat plate with different leading-edge shapes by means of particle image velocimetry and surface pressure measurements. Wind tunnel tests are performed in both smooth and various turbulent flow conditions, and the separated and reattaching flows are examined as a function of Reynolds number (Re), leading-edge shape, turbulence intensity, and turbulence integral length scale. It is shown through the particle image velocimetry and pressure measurements that the Reynolds number effect is significant regarding the mean vorticity field, but with little effect on the mean velocity field. For the effects of leading-edge shape, the distributions of pressure coefficients respond strongly to the change in leading-edge angle, and both the velocity (streamwise and vertical) and vorticity fields have a clear dependence on the leading-edge shape. For the effects of freestream turbulence, the mean pressure coefficient responds strongly to turbulence intensity, whereas the fluctuating and peak suction pressure coefficients are dependent on both turbulence intensity and integral length scale. The size of the separation bubble contracts aggressively with increasing turbulence intensity, but it remains approximately invariant in response to the change in turbulence scale in the tested range.
机译:本文通过颗粒图像测速和表面压力测量,对具有不同前缘形状的钝平板上的分离流和重新附着流进行了全面研究。风洞试验在光滑和各种湍流条件下均进行,分离和重新附着的气流作为雷诺数(Re),前沿形状,湍流强度和湍流积分长度标度的函数进行检查。通过粒子图像测速和压力测量表明,雷诺数效应对平均涡度场很重要,但对平均速度场影响很小。对于前缘形状的影响,压力系数的分布对前缘角度的变化有强烈的响应,并且速度(流向和垂直)和涡度场都对前缘形状有明显的依赖性。对于自由流湍流的影响,平均压力系数对湍流强度有很强的响应,而波动压力和峰值吸气压力系数则取决于湍流强度和整体长度尺度。分离气泡的大小会随着湍流强度的增加而急剧收缩,但在测试范围内,它会随着湍流尺度的变化而保持大致不变。

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