摘要
A new partitioning algorithm for Navier-Stokes equations in relative/absolute cylindrical-coordinate systems is developed, which base on the combination of Navier-Stokes equations in rotor area and stator area. For the calculation of subareas, high resolution third-order ENN scheme and implicit LU-SGS method are applied. Central investigation is focused on the grid connecting methods between rotor area and stator area and corresponding treatment for rotor-stator interaction. The partitioning algorithm developed in this paper is demonstrated by numerical simulation of a three stages axial flow compressor with inlet guide vane, the computed result shows good accordance with experimental data.
| 源语言 | 英语 |
|---|---|
| 页(从-至) | 211-215 |
| 页数 | 5 |
| 期刊 | Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica |
| 卷 | 25 |
| 期 | 2 |
| 出版状态 | 已出版 - 6月 2007 |
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