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The Effect of Freestream Turbulence Integral Length Scale on Junction Flow Behavior

机译:自由流湍流积分长度尺度对结流行为的影响

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Junction flow is a common feature in many flows of practical and natural importance. At the junction of a wall-mounted obstacle and the wall, significant unsteadiness exists due to the presence of the horseshoe vortex. This is a coherent vortex structure which forms in front of the leading edge of the obstacle and is wrapped around the obstacle by the incoming flow. In turbulent flow, the horseshoe vortex experiences highly unsteady and non-periodic large scale motions and breakdown events. This dynamic behavior contributes to significant dynamic pressure loading on the obstacle and augmented heat transfer on the local wall and leading edge surfaces. While recent studies of the horseshoe vortex have suggested that significant interaction may occur between freestream turbulence and the horseshoe vortex, the effect of freestream turbulence length scale on the behavior of the horseshoe vortex has not yet been systematically determined. This study investigates the effect of variation in streamwise integral turbulent length scale on the dynamics of the horseshoe vortex system in front of a symmetric wing for a range of Reynolds numbers, turbulence intensities, and integral length scales. Time-resolved stereo particle image velocimetry (SPIV) measurements show that for the range of parameters studied, unsteadiness in the junction is only affected by integral length scale under the conditions of low body thickness Reynolds number and large turbulence intensity. A vorticity tracking technique is used to show that this effect is due to the greater rate of impingement of large turbulence features at the wing leading edge with increased integral length scale under these conditions.
机译:结流是许多具有实际和自然重要性的流的共同特征。在壁挂障碍物和墙壁的交界处,由于存在马蹄涡流,因此存在很大的不稳定性。这是一个连贯的涡流结构,形成在障碍物前缘的前面,并被进入的气流包裹在障碍物周围。在湍流中,马蹄涡旋经历高度不稳定和非周期性的大规模运动和破坏事件。这种动态行为有助于显着增加障碍物上的动态压力负荷,并增加局部壁和前缘表面上的热量传递。尽管最近对马蹄形涡流的研究表明,自由流湍流和马蹄形涡流之间可能发生显着的相互作用,但尚未系统地确定自由流湍流长度尺度对马蹄形涡流行为的影响。这项研究调查了一系列雷诺数,湍流强度和积分长度尺度下,流向整体湍流长度尺度变化对对称翼前马蹄涡流系统动力学的影响。时间分辨立体粒子图像测速(SPIV)测量表明,对于所研究的参数范围,在低车身厚度雷诺数和大湍流强度的条件下,交界处的不稳定性仅受积分长度尺度的影响。涡度跟踪技术用于显示这种效果是由于在这些条件下,随着增大的整体长度尺度,机翼前缘处较大湍流特征的撞击率更高。

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