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EXPERIMENTAL INVESTIGATION OF BOUNDARY LAYER INSTABILITIES ON THE FREE SURFACE OF NON-TURBULENT JET

机译:非湍流射流自由表面上边界层不稳定性的实验研究

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Shear instabilities induced by the relaxation of laminar boundary layer at the free surface of a high speed liquid jet are investigated experimentally. Physical insights into these instabilities and the resulting capillary wave growth are gained by performing non-intrusive measurements of flow structure in the direct vicinity of the surface. The experimental results are a combination of surface visualization, planar laser induced fluorescence (PLIF), particle image velocimetry (PIV), and particle tracking velocimetry (PTV). They suggest that 2D span wise vortices in the shear layer play a major role in these instabilities by triggering 2D waves on the free surface as predicted by linear stability analysis. These vortices, however, are found to travel at a different speed than the capillary waves they initially created resulting in interference with the waves and wave growth. A new experimental facility was bui it consists of a 20.3×146.mm rectangular water wall jet with Reynolds number based on channel depth between 3.13 × 10~4 to 1.65 ×10~5 and 115. to 264. based on boundary layer momentum thickness.
机译:实验研究了层状边界层在高速液体射流自由表面上弛豫引起的剪切不稳定性。通过对表面直接附近的流动结构进行非侵入式测量,可以获得对这些不稳定性和由此产生的毛细管波增长的物理见解。实验结果是表面可视化,平面激光诱导荧光(PLIF),粒子图像测速(PIV)和粒子跟踪测速(PTV)的组合。他们认为,如线性稳定性分析所预测的那样,剪切层中的二维跨度涡旋通过在自由表面上触发二维波,在这些不稳定性中起主要作用。但是,发现这些涡流的传播速度与其最初产生的毛细管波的传播速度不同,从而导致对波的干扰和波的生长。建造了一个新的实验设施;它由一个20.3×146.mm矩形水冷壁射流组成,其雷诺数基于通道深度在3.13×10〜4至1.65×10〜5和115.至264.之间,基于边界层动量厚度。

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