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A vortex method suitable for long time simulations of flow over body of arbitrary geometry

机译:适用于长时间模拟任意几何体上的流动的涡旋方法

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摘要

In this paper, a core-spreading vortex method suitable for a long-time simulation of 2D flows over an immersed body of arbitrary shape is proposed. This vortex method employs the splitting and merging skills to control the convection error, imposes a vortex sheet on the body to enforce the no-slip boundary condition, selects a fast vortex method to speed up the computation, and finally takes advantage of the boundary element method to create the geometry flexibility. Several efforts have been made particularly in improving the long-time accuracy. Firstly, for the over-weak blobs generated during the blob splitting, we distribute their strength to nearby non-weak blobs through a near-to-far algorithm before removing them from the simulation. Secondly, we determine the appropriate approximation solution and optimize the discretization of the vortex sheet diffusion. Thirdly, to prevent blobs from staying too close to the wall, we define a proper near-wall region, which can be easily applied to arbitrarily shaped bodies, and exclude any blob from it. Finally, an outflow boundary condition is designed to control the total blob number. The flows induced by the impulsively started airfoil, circular, and elliptic cylinders are simulated and the accuracy and efficiency of the proposed vortex method are confirmed by the agreement of the present simulation results with those in the literatures.
机译:在本文中,提出了一种适用于长时间模拟任意形状的沉浸体上二维流动的堆芯扩散涡旋方法。这种涡流方法利用分裂和合并技巧来控制对流误差,在身体上施加涡流片以强制执行无滑移边界条件,选择一种快速涡流方法以加快计算速度,并最终利用边界元素创建几何灵活性的方法。特别是在提高长时间精度方面已经做出了一些努力。首先,对于在斑点分裂过程中产生的过度弱斑点,我们将其强度通过近距离算法分配给附近的非弱斑点,然后再将其从模拟中删除。其次,我们确定合适的近似解并优化涡旋片扩散的离散化。第三,为防止斑点过分靠近壁,我们定义了一个合适的近壁区域,该区域可轻松应用于任意形状的物体,并从中排除任何斑点。最后,设计了流出边界条件来控制总斑点数。模拟了由脉冲启动的翼型,圆形和椭圆形圆柱体引起的流动,并通过本模拟结果与文献的一致性证实了所提出的涡旋方法的准确性和效率。

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