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首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers >Integrated improvement of the elasticity-based mesh deformation method based on robust parameters and mesh quality
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Integrated improvement of the elasticity-based mesh deformation method based on robust parameters and mesh quality

机译:基于鲁棒参数和网格质量的基于弹性的网格变形方法的综合改进

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摘要

Highly robust mesh deformation methods are key techniques for solving unsteady flow field problems with moving or deforming boundaries. Because it is imperative to reduce the remeshing times, these methods are important in engineering applications, especially for complex geometric boundaries and large displacements. We introduce three classical elasticity-based mesh deformation methods and determine the limitations of the two nonlinear classical methods. Two steps were taken to achieve an integrated improvement: first, the robust power parameters a and b and the weighted parameter x are introduced to enhance the robustness of the basic elasticity equation. Second, a mesh quality parameter is implemented to prevent the large distortion of the poor elements and this parameter is added to the elasticity equation as a constraint. To validate the validity of the integrated improvement approach, several test cases of a moving or deforming two-dimensional flat plate are used. Additionally, two simulated engineering examples are used to demonstrate the application of the integrated improvement for practical problems, including the pitching oscillation of a National Advisory Committee for Aeronautics (NACA) 0012 airfoil and the ONERA M6 wing. The results show that the integrated improvement approach does not only allow for the selection of suitable robust parameters to achieve more robust deformed meshes but also reduces the distortion of the poor elements near the moving boundary, even when the deformation is severe.
机译:高度鲁棒的网格变形方法是解决边界移动或变形的非恒定流场问题的关键技术。由于必须减少重新网格化的时间,因此这些方法在工程应用中非常重要,尤其是对于复杂的几何边界和大位移而言。我们介绍了三种基于弹性的经典网格变形方法,并确定了两种非线性经典方法的局限性。采取了两个步骤来实现整体改进:首先,引入鲁棒功率参数a和b以及加权参数x以增强基本弹性方程的鲁棒性。其次,实施网格质量参数以防止不良元素的大变形,并将该参数作为约束添加到弹性方程中。为了验证集成改进方法的有效性,使用了移动或变形的二维平板的几个测试案例。此外,还使用两个模拟的工程实例来演示对实际问题进行综合改进的应用,包括国家航空咨询委员会(NACA)0012机翼和ONERA M6机翼的俯仰振动。结果表明,综合改进方法不仅允许选择合适的鲁棒参数以实现更鲁棒的变形网格,而且即使在变形严重的情况下,也可以减少移动边界附近的不良元素的变形。

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