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Large Eddy Simulation of Flow over a Twisted Elliptic Cylinder at a Subcritical Reynolds Number

机译:亚临界雷诺数下椭圆形圆柱上绕流的大涡模拟

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The wavy cylinder has a sinusoidal variation in cross sectional area along the spanwise direction and the torsional cylinder has been newly designed by rotating the elliptic cross section along the spanwise direction, so that the cylinder surface has a twisted spiral pattern. For an ellipse, different eccentricities are considered to observe the effect of eccentricity on the flow fields. It guarantees the accuracy of the present numerical methods that the excellent comparisons with previous studies for the cases of a smooth circular cylinder and a wavy cylinder. The effect of surface torsion which is newly designed in here has been predicted and assessed in terms of the mean drag and root-mean-square (RMS) value of fluctuating lift in the subcritical Reynolds number range. Subsequently, the mechanisms of enhancing the aerodynamic performance and passive control of vortex-induced vibrations are also investigated by careful analysis with the flow structures. The isosurface of swirling strength has been imposed to identify the vortical structures in the turbulent wake.
机译:波浪圆柱体沿翼展方向具有截面积的正弦变化,并且扭转圆柱体是通过沿椭圆展向旋转椭圆形截面而新设计的,因此圆柱体表面具有扭曲的螺旋图案。对于椭圆,考虑不同的偏心率以观察偏心率对流场的影响。它保证了当前数值方法的准确性,与光滑圆柱体和波浪圆柱体情况下的先前研究进行了出色的比较。在亚临界雷诺数范围内,根据波动的升力的平均阻力和均方根(RMS)值,可以预测和评估此处新设计的表面扭转效果。随后,还通过对流动结构进行仔细分析,研究了增强空气动力性能和被动控制涡流引起的振动的机制。为了确定湍流尾流中的旋涡结构,已施加等强度的旋流强度。

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