摘要
A method for generating three-dimensional mixed-element-type unstructured grids and its application in simulating viscous flow by solving the Navier-Stokes equations are presented. Pirzadeh's advancing-layer method is modified to generate high-quality mixed prismatic/pyramid/ tetrahedral-element-type unstructured grids in the boundary-layer region, and the traditional advancing-front method is used to construct isotropic tetrahedral grids in the residual flow region. Based on the Spalart-Allmaras one equation turbulence model, three-dimensional Navier-Stokes equations are solved by using a cell-centered finite-volume method. Viscous flow problems around the ONERA M6 wing, a DLR-F4 wing-body configuration and a transport configuration are simulated to verify the correctness and practicability of the methods.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 385-390 |
| 页数 | 6 |
| 期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
| 卷 | 24 |
| 期 | 5 |
| 出版状态 | 已出版 - 9月 2003 |
指纹
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