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Effects of Vertical Position and Orientation on a Vortical-Gust/Airfoil Interaction at a Transitional Reynolds Number

机译:垂直位置和取向对过渡雷诺数下涡流/阵风/机翼相互作用的影响

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This article presents high-fidelity implicit large eddy simulations (ILES) of parallel vortical gust interactions with a NACA0012 airfoil operating at a transitional Reynolds number of Re_c = 200,000 and an angle of attack of α = 4°. The gust is supplied upstream of the airfoil as a Taylor vortex. Three different initial vertical positions are considered for a counterclockwise-oriented gust as well as one vertical position for a clockwise-oriented gust. In all cases, the unsteady flow is explored in detail elucidating characteristic behaviors and their effects on aerodynamic loading. Both the upper and lower surface boundary layers are shown to produce a very different response and recovery depending on the vertical position or orientation of the incoming gust. Acoustic sources specific to gust-induced viscous flow events and common to either gust orientation are identified and merit further study.
机译:本文介绍了在过渡雷诺数Re_c = 200,000和迎角α= 4°的条件下运行的NACA0012翼型的平行涡旋阵风相互作用的高保真隐式大涡模拟(ILES)。阵风以泰勒涡旋的形式在机翼上游提供。对于逆时针方向的阵风,考虑了三个不同的初始垂直位置,对于顺时针方向的阵风,考虑了一个垂直位置。在所有情况下,都将详细研究非稳态流动,以阐明特征行为及其对空气动力学载荷的影响。上表面边界层和下表面边界层都显示出很大的响应和恢复,具体取决于传入阵风的垂直位置或方向。识别出特定于阵风引起的粘性流动事件并且对于阵风取向通用的声源,并值得进一步研究。

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