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首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >Characteristic length scales for vortex detachment on plunging profiles with varying leading-edge geometry
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Characteristic length scales for vortex detachment on plunging profiles with varying leading-edge geometry

机译:具有变化的前沿几何形状的插入轮廓上的涡旋分离的特征长度标尺

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Experiments on leading-edge vortex (LEV) growth and detachment from a plunging profile have been conducted in a free-surface water tunnel. Direct-force and velocity-field measurements have been performed at a Reynolds number of Re = 10,000, a reduced frequency of k = 0.25, and a Strouhal number of St = 0.16, for three varying leading-edge geometries. The leading-edge shape is shown to influence the shear layer feeding the LEV, and thus to some extent the development of the LEV and associated flow topology. This effect in turn influences the arrival time of the rear (LEV) stagnation point at the trailing edge, which, once breached, constitutes a detachment of the LEV. It is found that despite minor phase changes in LEV detachment through leading-edge shape, the position of the trailing edge (chord length) should be chosen as the characteristic length scale for the vortex separation process.
机译:在自由表面水隧道中进行了前沿涡流(LEV)的生长和从下降剖面中脱离的实验。对于三种不同的前沿几何形状,已经在Re = 10,000的雷诺数,k = 0.25的降低频率以及St = 0.16的Strouhal数的情况下执行了直接力和速度场测量。示出的前缘形状影响供给LEV的剪切层,并因此在某种程度上影响LEV的发展和相关的流动拓扑。反过来,这种影响会影响后(LEV)停滞点到达后缘的时间,一旦停顿,该停滞点一旦被破坏就构成LEV的分离。发现尽管通过前缘形状LEV脱离的相位变化很小,但应选择后缘的位置(弦长)作为涡旋分离过程的特征长度尺度。

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