Title of article :
A novel approach of three-dimensional hybrid grid methodology: Part 2. Flow solution Original Research Article
Author/Authors :
Meng-Sing Liou، نويسنده , , Bangti Jin and Yao Zheng، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2003
Pages :
21
From page :
4173
To page :
4193
Abstract :
Following the previous paper of this series, which addresses the generation approach of three-dimensional DRAGON grids, we demonstrate the capability of effectively performing three-dimensional flow calculations for multi-components complex configurations. The flow solution is conducted by means of using a seamlessly integrated package made up of two well-validated NASA solvers, which are structured- and unstructured-grid codes, respectively.
Keywords :
Turbine vanes , Cascade flow , Turbomachinery , Supersonic flow , Subsonic flow , Computational fluid dynamics , Flow solution , AUSM scheme , Hybrid grid , Viscous flow
Journal title :
Computer Methods in Applied Mechanics and Engineering
Serial Year :
2003
Journal title :
Computer Methods in Applied Mechanics and Engineering
Record number :
892860
Link To Document :
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