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Geometric Perturbations and Asymmetric vortex shedding About Slender Pointed Bodies

机译:细长尖体的几何扰动和不对称涡旋脱落

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摘要

The flow about slender, pointed bodies can be characterized by different states with angle of attack. At moderate-to-high angles of attack (alpha approximately equals 40deg), a steady, asymmetric vortex pattern develops along the body, leading to a net lateral force. At higher angles of attack (alpha approximately equals 60deg), the aft-end of the body develops an unsteady von Karman shedding. As the angle of attack approaches 90deg, the entire body length exhibits a time-dependent vortex shedding pattern. The current work uses three-dimensional, thin-layer Navier-Stokes simulations to investigate the physical mechanisms of asymmetric vortex shedding at alpha = 40deg and alpha = 60deg. The development of an asymmetric vortex pattern via a convective instability mechanism is investigated using tip bumps, surface roughness, and tip curvature. It's found that surface roughness simulations can incite an asymmetric vortex state at alpha = 60deg which is consistent with the application of a tip bumps, and the experimentally observed flowfield. The unsteady von Karman vortex shedding on the aft portion of the body is also well resolved. The use of surface roughness did not incite a flow asymmetry at alpha = 40deg, and it was necessary to simulate tip curvature at this angle of attack in order to generate an asymmetric vortex state.
机译:细长的,尖锐的物体周围的流动的特征是具有迎角的不同状态。在中等到高的迎角(α大约等于40度)处,沿着身体会形成稳定的不对称涡旋图案,从而导致净侧向力。在较高的迎角(α大约等于60度)下,身体的尾端会出现不稳定的von Karman脱落。当迎角接近90度时,整个身体的长度呈现出随时间变化的涡旋脱落模式。当前的工作使用三维薄层Navier-Stokes模拟来研究α= 40度和α= 60度时非对称涡旋脱落的物理机理。研究了通过对流不稳定性机制通过不对称涡旋图案的发展,其中利用了尖端凸起,表面粗糙度和尖端曲率。已经发现,表面粗糙度模拟可以在α= 60deg处引发不对称的涡旋状态,这与施加尖峰和实验观察到的流场一致。人体后部部分的不稳定von Karman涡旋脱落也得到了很好的解决。使用表面粗糙度不会在alpha = 40deg时引起流动不对称,并且有必要在此迎角下模拟尖端曲率,以产生不对称的涡旋状态。

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