Rapid meshing of turbomachinery rows using semi-unstructured multi-block conformal grids

被引：17

作者：

Burgos, Manuel A. ^{[1
]}

Chia, Juan M. ^{[2
,3
]}

Corral, Roque ^{[2
,3
]}

Lopez, Carlos ^{[2
,3
]}

机构：

[1] Univ Politecn Cartagena, Cartagena 30202, Spain

[2] Ind TurboPropulsores SA, Madrid 28830, Spain

[3] ITP, Madrid, Spain

来源：

ENGINEERING WITH COMPUTERS | 2010年 / 26卷 / 04期

关键词：

Grid; Hybrid; Delaunay; Semi-unstructured; Turbomachinery;

D O I：

10.1007/s00366-009-0169-7

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

A semi-unstructured grid generation method especially tailored for the meshing of turbomachinery blade passages and their associated cavities is presented. The method is based on a smart combination of quasi-3D methods, an ad hoc block decomposition of the domain and a grid-based solid-model-less reconstruction of the computational domain.

引用

页码：351 / 362

页数：12

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