A deformable overset grid method is proposed to simulate the unsteady aerodynamic problems with multiple flexible moving bodies. This method uses an unstructured overset grid coupled with local mesh deformation to achieve both robustness and efficiency. The overset grid hierarchically organizes the subgrids into clusters and layers, allowing for overlapping/embedding of different type meshes, in which the mesh quality and resolution can be independently controlled. At each time step, mesh deformation is locally applied to the subgrids associated with deforming bodies by an improved Delaunay graph mapping method that uses a very coarse Delaunay mesh as the background graph. The graph is moved and deformed by the spring analogy method according to the specified motion, and then the computational meshes are relocated by a simple one-to-one mapping. An efficient implicit hole-cutting and intergrid boundary definition procedure is implemented fully automatically for both cell-centered and cell-vertex schemes based on the wall distance and an alternative digital tree data search algorithm. This method is successfully applied to several complex multibody unsteady aerodynamic simulations, and the results demonstrate the robustness and efficiency of the proposed method for complex unsteady flow problems, particularly for those involving simultaneous large relative motion and self-deformation.ududud
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机译:提出了一种可变形的覆盖网格方法来模拟具有多个柔性运动体的非定常空气动力学问题。该方法使用非结构化的偏心网格加上局部网格变形来实现鲁棒性和效率。覆盖网格按层次结构将子网格组织为簇和层,从而允许重叠/嵌入不同类型的网格,其中网格质量和分辨率可以独立控制。在每个时间步,通过使用非常粗糙的Delaunay网格作为背景图的改进的Delaunay图映射方法,将网格变形局部应用于与变形体关联的子网格。通过弹簧类比方法根据指定的运动来移动和变形图形,然后通过简单的一对一映射来重新定位计算网格。基于壁距和可选的数字树数据搜索算法,针对以细胞为中心和以细胞为顶点的方案,可以完全自动地执行有效的隐式孔切割和网格间边界定义过程。该方法成功地应用于几种复杂的多体非定常空气动力学模拟,结果证明了该方法对于复杂的非定常流动问题的鲁棒性和效率,特别是对于那些同时存在较大的相对运动和自变形的问题。 ud ud ud
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