摘要
Numerical simulation to three-dimensional turbulent flow in multistage axial compressor blade row is carried out, where high resolution third-order ENN scheme is adopted to catch the shockwave and simulate the turbulent flow correctly, and LU-SGS implicit method is chosen to improve computation rate. A nicety and high efficiency numerical simulating system is thus constructed. Central investigation is focused on the grid connecting methods between rotor and stator and the corresponding treatment for rotor-stator interactional surface. The final results for a three stages axial compressor with inlet guide vane show good accordance with the experimental data.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 21-25 |
| 页数 | 5 |
| 期刊 | Yingyong Lixue Xuebao/Chinese Journal of Applied Mechanics |
| 卷 | 24 |
| 期 | 1 |
| 出版状态 | 已出版 - 3月 2007 |