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Advanced Unstructured Grid Generation for Complex Aerodynamic Applications

机译:先进的非结构化网格生成,适用于复杂的气动应用

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摘要

A new approach for the distribution of grid points on the surface and in the volume has been developed. In addition to the point and line sources of previous works, the new approach uses surface and volume sources for automatic curvature-based grid sizing and convenient point distribution in the volume. A new exponential growth function produces smoother and more efficient grids and provides superior control over the distribution of grid points in the field. All types of sources support anisotropic grid stretching, which not only improves the grid economy but also provides more accurate solutions for certain aerodynamic applications. The new approach does not require a three-dimensional background grid as in the previous methods. Instead, it makes use of an efficient bounding-box auxiliary medium for storing grid parameters defined by surface sources. The new approach is less memory intensive and more efficient computationally. The grids generated with the new method either eliminate the need for adaptive grid refinement for certain class of problems or provide high-quality initial grids that would enhance the performance of many adaptation methods.
机译:已经开发出一种在表面和体积中分布网格点的新方法。除了先前工作中的点和线源外,新方法还使用了面和体源,以基于曲率的自动网格大小调整和方便地在体中分布点。新的指数增长函数可生成更平滑,更高效的网格,并提供对现场网格点分布的出色控制。所有类型的源均支持各向异性网格拉伸,这不仅可以提高网格经济性,还可以为某些空气动力学应用提供更准确的解决方案。与以前的方法一样,新方法不需要三维背景网格。取而代之的是,它利用有效的包围盒辅助介质来存储由表面源定义的网格参数。新方法的内存占用较少,计算效率更高。用新方法生成的网格要么不需要针对某些类型的问题进行自适应网格优化,要么提供可以提高许多自适应方法性能的高质量初始网格。

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