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AERODYNAMIC FORCES ON A ROTATING SPHERE AT REYNOLDS NUMBER AROUND THE DRAG CRISIS REGION

机译:在拖累危机区周围雷诺数的旋转球体上的空气动力

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Flow characteristics and fluid force on a sphere rotating along with axis perpendicular to mean air flow are investigated using Large Eddy Simulation at three Reynolds numbers of 10~4, 2.0*10~5 and 2.4*10~5. Particular attention has been devoted to a prediction of rotation effect on a promotion of boundary layer transition around the sphere. As a result of simulation, a change of velocity profile around the sphere and displacement of the separation point are visualized. When sphere rotates at Reynolds numbers of 10~4, flow characteristics agree with the flow field explained in the Magnus effect. While sphere rotates at Reynolds numbers of 2.0*10~5, separation point and wake direction are opposite to Reynolds numbers of 10~4 case, and these flow aspects agree with characteristics explained in the negative Magnus effect.
机译:使用大涡流模拟在三个雷诺数为10〜4,2.0 * 10〜5和2.4 * 10〜5的情况下使用大涡流旋转与垂直于平均气流的球体上的流体特性和流体力。特别注意对球体周围边界层转变的旋转效果的预测。由于模拟的结果,可视化分离点的球体周围的速度曲线的变化和位移。当球体在雷诺数为10〜4时旋转​​时,流动特性与Magnus效果中解释的流场一致。虽然球体在2.0 * 10〜5的雷诺数时旋转,但分离点和唤醒方向与10〜4例的雷诺数相反,并且这些流动方面与负数大效应中解释的特征一致。

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