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Adaptive unstructured triangular mesh generation and flow solvers for the Navier-Stokes equations at high Reynolds number

机译:高雷诺数下Navier-Stokes方程的自适应非结构​​化三角形网格生成和流动求解器

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摘要

A method for generating high quality unstructured triangular grids for high Reynolds number Navier-Stokes calculations about complex geometries is described. Careful attention is paid in the mesh generation process to resolving efficiently the disparate length scales which arise in these flows. First the surface mesh is constructed in a way which ensures that the geometry is faithfully represented. The volume mesh generation then proceeds in two phases thus allowing the viscous and inviscid regions of the flow to be meshed optimally. A solution-adaptive remeshing procedure which allows the mesh to adapt itself to flow features is also described. The procedure for tracking wakes and refinement criteria appropriate for shock detection are described. Although at present it has only been implemented in two dimensions, the grid generation process has been designed with the extension to three dimensions in mind. An implicit, higher-order, upwind method is also presented for computing compressible turbulent flows on these meshes. Two recently developed one-equation turbulence models have been implemented to simulate the effects of the fluid turbulence. Results for flow about a RAE 2822 airfoil and a Douglas three-element airfoil are presented which clearly show the improved resolution obtainable.
机译:描述了一种用于为有关复杂几何形状的高雷诺数Navier-Stokes计算生成高质量非结构化三角网格的方法。在网格生成过程中要格外注意,以有效地解决这些流中出现的不同长度尺度。首先,以确保真实表示几何形状的方式构造表面网格。然后,体积网格的生成分两个阶段进行,因此可以使流的粘性区域和不粘稠区域最佳地网格化。还描述了一种解决方案自适应的重新网格化过程,该过程允许网格自身适应流动特征。描述了跟踪尾波的过程和适合震动检测的细化标准。尽管目前仅在两个维度上实现,但在设计网格生成过程时要考虑到三个维度的扩展。还提出了一种隐式的高阶迎风方法,用于计算这些网格上的可压缩湍流。已经实施了两个最近开发的一方程湍流模型来模拟流体湍流的影响。给出了有关RAE 2822机翼和道格拉斯三元翼型的流场结果,清楚地表明可获得提高的分辨率。

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