Automatic unstructured surface mesh generation for complex configurations

被引:14
|
作者
Tremel, U
Deister, F
Hassan, O [1 ]
Weatherill, NP
机构
[1] Univ Coll Swansea, Sch Engn, Civil Computat Engn Ctr, Swansea SA2 8PP, W Glam, Wales
[2] EADS Mil Aircraft, Flight Phys Dept, D-81663 Munich, Germany
关键词
D O I
10.1002/fld.671
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
In this paper a new object-oriented (OO) approach is presented for automatic parallel advancing front based surface mesh generation and adaptive remeshing for complex configurations. Based on the ST++-system the advantages of the OO design and implementation compared to the traditional structural approach are described. Algorithmic enhancements to the advancing front method are explained, enabling a robust NURBS based triangulation process directly on B-rep CAD data. The message passing (MPI) parallelization strategy together with the achievable performance improvements are demonstrated. With the outlined parallel geometry analysis/rasterization a powerful method is described to derive automatically a well suited mesh size specification without any user-interaction from scratch. The application of this method to a complex 'real world' example finishes this paper. Copyright (C) 2004 John Wiley Sons, Ltd.
引用
收藏
页码:341 / 364
页数:24
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