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Aeroelastic interactions and trajectory selection of vortex gusts impinging upon Joukowski airfoils

机译:涡旋阵风的空气弹性相互作用与轨迹选择抵抗joukowski翼型

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摘要

The dynamically-coupled interactions of vortex gusts encountering a symmetric Joukowski airfoil on linear elastic supports is formulated analytically and evaluated numerically using a time-dependent conformal mapping. The Brown and Michael framework models the unsteady shedding of vorticity from the airfoil into the wake, and the aeroelastic motion of the airfoil is analyzed using quasi-steady, apparent mass, and fully-unsteady aerodynamic models. Special attention is paid to the influences of the strength of the incident vortex and the airfoil natural frequency on the initial upstream placement of a vortex gust that achieves direct impingement. These results are weakly sensitive to the initial vortex position in the limits of either large or small structural natural frequency, and the initial vertical vortex position to achieve impingement changes monotonically with the vortex strength. A comparison of the numerical model with available experimental vortex gust measurements over stationary airfoils highlights the appropriate use of the point-vortex model for inviscid vortex-airfoil interaction problems without significant vortex strength decay, which occurs for predominantly viscous interactions of close vortex-airfoil encounters. (C) 2020 Elsevier Ltd. All rights reserved.
机译:在线性弹性支撑件遇到对称joukowski翼型的涡旋阵风的动态耦合相互作用在线性弹性支撑体配制,并使用时间依赖的保形映射进行数值评估。棕色和迈克尔框架模型模型从翼型旋翼进入唤醒,翼型的空气弹性运动使用准稳态,表观质量和完全不稳定的空气动力学模型进行分析。特别注意事件涡流强度和翼型固有频率对涡旋阵风的初始上游放置,实现直接冲击的影响。这些结果对大大或小结构自然频率的限制中的初始涡流位置弱敏感,并且初始垂直涡流位置以涡流强度单调地实现冲击变化。在固定翼型上的可用实验涡旋阵风测量的数值模型的比较突出了不显着的涡旋强度衰减的抗体涡旋 - 翼型相互作用问题的适当用途,这发生了密切涡流的粘性相互作用的主要粘性相互作用。 (c)2020 elestvier有限公司保留所有权利。

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