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Aerodynamic Coefficients of a Spinning Sphere in a Rarefied-Gas Flow

机译:稀薄气体流中自旋球体的空气动力学系数

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A three-dimensional rarefied-gas flow past a spinning sphere in the transitional and near-continuum flow regimes is studied numerically. The rarefaction and compressibility effects on the lateral (Magnus) force and the aerodynamic torque exerted on the sphere are investigated for the first time. The coefficients of the drag force, the Magnus force, and the aerodynamic torque are found for Mach numbers ranging from 0.1 to 2 and Knudsen numbers ranging from 0.05 to 20. In the transitional regime, at a certain Knudsen number depending on the Mach number the Magnus force direction changes. This change is attributable to the increase in the role of normal stresses and the decrease in the contribution of the shear stresses to the Magnus force with decrease in the Knudsen number. A semi-empirical formula for the calculation of the Magnus force coefficient in the transitional flow regime is proposed.
机译:数值研究了过渡和近连续流动状态下通过旋转球体的三维稀有气体流。首次研究了对横向(马格努斯)力和施加在球体上的空气动力学扭矩的稀疏性和可压缩性影响。对于范围为0.1到2的马赫数和范围为0.05到20的克努森数,发现了阻力,马格努斯力和空气动力学扭矩的系数。在过渡状态下,根据马赫数,在一定的克努森数下,马格努斯力方向发生变化。这种变化可归因于法向应力作用的增加以及剪切应力对马格努斯力的贡献的减小(随克努森数的减小)。提出了计算过渡流态马格努斯力系数的半经验公式。

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