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Structural analysis on a hemisphere-cylinder at moderate Reynolds number and high angle of attack

机译:雷诺数中等和高攻角的半球圆柱体的结构分析

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Three-dimensional DNS has been performed on a hemisphere-cylinder at Reynolds number Re= 1000 and angle of attack AoA= 20° in order to analyze flow structures and wake frequencies. PIV experiments have also been carried out over the same geometry and flow conditions to validate the numerical results. Critical point theory has been applied in order to determine the topology patterns over the surface of the body. Critical points and separation lines on the body surface show the presence of three different flow patterns: separation bubble, "horn vortices" and "leeward vortices". Both, "horn vortices" and "leeward vortices" are found to be asymmetric and unsteady. The frequency related to "leeward vortices" oscillations has been identified both experimentally and numerically. Two more dominant frequencies, related to two different wake shedding modes have been found. On the other hand, POD has been performed and the four most energetic POD modes is found to be composed of a mixture of these three frequencies. They are modes on the wake shedding. Finally, DMD modes associated with these three frequencies are found on the symmetry plane close to the nose area. These modes represent different shear layer instabilities. Flow separation was found to be intrinsically linked with the observed shear-layer instability.
机译:为了分析流动结构和尾流频率,已经在雷诺数Re = 1000和迎角AoA = 20°的半球圆柱体上执行了三维DNS。还对相同的几何形状和流动条件进行了PIV实验,以验证数值结果。为了确定人体表面的拓扑结构,已应用了临界点理论。体表上的临界点和分离线表明存在三种不同的流动模式:分离气泡,“角涡”和“下风涡”。发现“喇叭形涡旋”和“下风涡旋”都是不对称且不稳定的。在实验和数值上都已经确定了与“背风涡”振荡有关的频率。已经发现了与两个不同的尾流脱落模式有关的另外两个主导频率。另一方面,已经执行了POD,发现四个最有活力的POD模式是由这三个频率的混合组成的。它们是唤醒后的模式。最后,在靠近鼻子区域的对称平面上发现了与这三个频率相关的DMD模式。这些模式代表了不同的剪切层不稳定性。发现流动分离与观察到的剪切层不稳定性有内在联系。

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