摘要
A two-dimensional Navier-Stokes equation was solved to predict unsteady flow and temperature fields with different turbulence intensity in a turbine stage. It is found that turbulence intensity has significant effects on the temperature distribution but the pressure distribution does not. When hot streak was introduced in the turbine's inlet, high turbulence intensity would make the temperature of hot gas diffuse more quickly, and the temperature distribution tend to be more uniform. The temperature discrepancy between suction surface and pressure surface of rotor would be decreased, and the temperature profile along the chord become more even.
| 源语言 | 英语 |
|---|---|
| 页（从-至） | 40-44 |
| 页数 | 5 |
| 期刊 | Tuijin Jishu/Journal of Propulsion Technology |
| 卷 | 23 |
| 期 | 1 |
| 出版状态 | 已出版 - 2月 2002 |