Influence of pulsating frequencies on characteristic of radial turbine rotor inlet flow

被引:0
|
作者
Wang Z. [1 ,2 ]
Ma C. [1 ]
Zhu F. [1 ]
机构
[1] School of Mechanical Engineering, Beijing Institute of Technology, Beijing
[2] Department of Mechanics, Jinzhong University, Jinzhong
来源
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2021年 / 36卷 / 03期
关键词
Flow angle; Pulsating flow; Pulsating frequency; Radial variable nozzle turbine; Rotor inlet;
D O I
10.13224/j.cnki.jasp.2021.03.020
中图分类号
学科分类号
摘要
Detailed understanding of the flow interaction within the complex geometry of turbine stage coupled with the imposed unsteady pressure waves was presented. A fully validated numerical model was established based on ANSYS CFX code. For this purpose, four unsteady simulations of 20, 40, 60 and 80Hz together with the steady state simulations were conducted. The flow angle distribution in a pulsating cycle and at the circumferential and spanwise positions was analyzed in different pulsating frequency conditions. The results showed that the pulsating frequency mainly affected the inlet incidence angle of rotor at the high pressure side, moreover, the lower the pulse frequency, the greater the negative incident angle of the low pressure side. It was also found that the absolute flow angle distribution at circumferential potion was similar and the relative flow angle fluctuations during the pressure decrements instances was significantly lower as compared with that during pressure increment instances. © 2021, Editorial Department of Journal of Aerospace Power. All right reserved.
引用
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页码:646 / 654
页数:8
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