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首页> 外文期刊>Bulletin of the American Physical Society >APS -70th Annual Meeting of the APS Division of Fluid Dynamics- Event - Vorticity dynamics of revolving wings: The role of planetary vortex tilting on the stability of leading-edge vortex
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APS -70th Annual Meeting of the APS Division of Fluid Dynamics- Event - Vorticity dynamics of revolving wings: The role of planetary vortex tilting on the stability of leading-edge vortex

机译:APS-APS流体动力学分部第70届年会-事件-旋转机翼的涡旋动力学:行星涡旋倾斜对前沿涡旋稳定性的作用

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This work investigates the radial vorticity dynamics and the stability of leading-edge vortices (LEVs) in revolving wings. Previous studies have shown that Coriolis acceleration plays a key role in stabilizing the LEV; however, the exact mechanism remains unclear. This study tests a new hypothesis based on the curl of the Coriolis acceleration in the vorticity equation, which corresponds to the radial tilting of the planetary vortex (PVTr). The PVTr could reorient planetary vorticity into radial vorticity that reduces the strength of the LEV, preventing the LEV from growing and becoming unstable. To test this, an in-house immersed-boundary-method-based flow solver was used to generate velocity and vorticity fields of revolving wings of different aspect ratio (AR $=$ 3, 5, 7) and Reynolds number (Re $=$ 110, 1400). It is found that the PVTr consistently negates the LEV vorticity for all the AR and Re investigated, although its effect is outweighed by other 3D effects at Re $=$1400. It is also found that the strength of the PVTr increases along the wing span until approximately a chord length from the wing tip. The averaged magnitude of PVTr within the LEV and the dependency of its relative strength on the aspect ratio and Reynolds number are also investigated.
机译:这项工作研究了径向旋涡动力学和旋转翼中前沿旋涡(LEV)的稳定性。先前的研究表明,科里奥利加速在稳定LEV中起着关键作用。但是,确切的机制仍不清楚。这项研究基于涡度方程中科里奥利加速度的卷曲,测试了一个新的假设,这对应于行星涡旋(PVTr)的径向倾斜。 PVTr可以将行星涡旋重新定向为径向涡旋,从而降低LEV的强度,从而防止LEV增长并变得不稳定。为了对此进行测试,使用了基于内部浸入边界方法的流动求解器来生成不同纵横比(AR $ = $ 3、5、7)和雷诺数(Re $ = $ 110,1400)。发现PVTr始终抵消所有AR和Re的LEV涡度,尽管在Re $ = $ 1400时,其其他3D效果远胜于PVTr。还发现PVTr的强度沿机翼跨度增加,直到距机翼尖端约弦长为止。还研究了LEV内PVTr的平均大小及其相对强度对长宽比和雷诺数的依赖性。

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