首页> 外文期刊>Aerospace science and technology >Unstructured 2D grid generation using overset-mesh cutting and single-mesh reconstruction
【24h】

Unstructured 2D grid generation using overset-mesh cutting and single-mesh reconstruction

机译:使用覆盖网格切割和单网格重建的非结构化2D网格生成

获取原文
获取原文并翻译 | 示例
       

摘要

In this paper a new approach for merging overlapping grids for CFD simulations is presented. The proposed strategy is a preprocessor that integrates the overset meshes into a single mesh suitable for unstructured finite volume vertex-centered Navier-Stokes solvers. This strategy aims to deal with complex industrial problems, specially in case of moving components and overlapping boundary layers. The algorithm consists of two key steps: the definition of a hole cutting area over each component mesh, where nodes of the other mesh are removed, and the subsequent remeshing of the gap generated between both meshes. In this process, the first issue is particularly critical and it employs auxiliary coarse Cartesian meshes to simplify the involved computations like wall distance calculations or point inclusion test. The proposed approach has been demonstrated on 2D test configurations using the DLR-TAU solver (C) 2018 Published by Elsevier Masson SAS.
机译:在本文中,提出了一种用于CFD仿真的合并重叠网格的新方法。所提出的策略是一种预处理器,它将过剩的网格集成到适合非结构化有限体积顶点为中心的Navier-Stokes求解器的单个网格中。该策略旨在处理复杂的工业问题,特别是在移动部件和重叠边界层的情况下。该算法包括两个关键步骤:在每个组件网格上定义一个孔切割区域,其中另一个网格的节点被删除,以及随后重新网格化两个网格之间生成的间隙。在这个过程中,第一个问题特别关键,它使用辅助的粗笛卡尔网格来简化所涉及的计算,例如壁距计算或点包含测试。已使用Elsevier Masson SAS发布的DLR-TAU求解器(C)2018在2D测试配置上演示了该方法。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号