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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 - The convective behavior of a dynamic stall vortex at low Reynolds number
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APS -70th Annual Meeting of the APS Division of Fluid Dynamics- Event - The convective behavior of a dynamic stall vortex at low Reynolds number

机译:APS-流体动力学APS部门第70届年会-事件-低雷诺数下动态失速涡流的对流行为

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摘要

Dynamic stall is a fundamental flow phenomenon that is commonly observed in biological flight and rotorcraft. Under certain conditions a leading edge vortex forms generating large but temporary lift forces. A common assumption for the convective behavior of the dynamic stall vortex (DSV) is that it convects downstream after forming and diffuses while convecting away. However, experiments on a NACA 0012 full span wing at Reynolds number of 12,000 showed the dynamic stall vortex undergoing a behavior that did not resemble diffusion as it convected downstream. Instead, the DSV was observed to compress in a specific region downstream of the wing. A comparison between the DSV behavior and convection of bluff body shedding, which occurred after the DSV was no longer present will be shown. A better understanding of this vortex breakdown method for the dynamic stall vortex at low Reynolds number may help improve vortex methods and CFD for studying dynamic stall.
机译:动态失速是一种基本的流动现象,通常在生物飞行和旋翼飞机中观察到。在某些情况下,会形成前缘涡流,从而产生较大但暂时的升力。动态失速涡流(DSV)的对流行为的一个常见假设是,它在形成后对流对流并在对流时扩散。但是,在雷诺数为12,000的NACA 0012全跨度机翼上进行的实验表明,动态失速涡流的行为与向下游对流时的扩散过程并不相似。相反,观察到DSV在机翼下游的特定区域压缩。将显示DSV行为和钝体脱落对流之间的比较,后者在DSV不再存在后发生。对于低雷诺数下的动态失速涡旋,这种涡旋分解方法的更好理解可能有助于改进研究动态失速的涡旋方法和CFD。

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