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Pressure measurements on the impingement surface of sonic and sub-sonic jets impinging onto a flat plate at inclined angles

机译:以倾斜角度撞击平板的音速和亚音速射流的撞击表面上的压力测量

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The flow field associated with a jet impinging onto a surface at an inclined angle is investigated using pressure-sensitive paint (PSP) and particle image velocimetry. The PSP yields continuous measurements of pressure on the jet impingement surface. The jet footprint on the impingement surface is visualized using the half-maximum pressure contour. The results indicate that the impingement angle of the jet is the dominant parameter in determining the footprint of the jet on the impingement surface. This contour is similar in shape to an ellipse that is created by projecting the nozzle through the impingement surface. The ellipse is centered at the location of maximum pressure and the width of the minor axis is just over one jet diameter. The location of maximum pressure is found upstream of the geometric impingement point and this location is a strong function of the impingement angle. A curve fit for the location of maximum pressure can be constructed using an exact solution of the Navier–Stokes equations for a non-orthogonal stagnation flow. The maximum value of pressure is a function of impingement angle and varies as the sine of the impingement angle squared; the maximum pressure is also a function of jet impingement distance. Using these results, a simple procedure for predicting the overall structure of the jet on the impingement surface is presented.
机译:使用压敏涂料(PSP)和颗粒图像测速技术研究了与以倾斜角度撞击表面的射流相关的流场。 PSP可连续测量射流冲击表面上的压力。冲击表面上的射流足迹可通过半最大压力轮廓显示。结果表明,射流的撞击角是确定射流在撞击表面上的足迹的主要参数。该轮廓的形状类似于椭圆形,该椭圆形是通过将喷嘴从撞击表面中伸出而形成的。椭圆位于最大压力的中心,短轴的宽度刚好超过一个喷嘴直径。在几何撞击点的上游发现最大压力的位置,并且该位置是撞击角度的强函数。对于非正交停滞流,可以使用Navier–Stokes方程的精确解来构造适合最大压力位置的曲线。压力的最大值是冲击角的函数,并随冲击角的正弦平方变化。最大压力也是射流冲击距离的函数。利用这些结果,提出了一种简单的方法来预测撞击表面上射流的整体结构。

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