本文利用数值方法研究了某两级低速轴流压气机第二级动叶在存在前后静叶扰动时,工况变化对其顶部非定常泄漏流波动频率的影响.结果显示其波动主要集中在泄漏涡轨迹附近,并且随着流量减小而增强.在大流量工况,其波动频率为转子通道频率.在中等流量工况,其波动频率为0.59倍通道频率.在小流量工况,其波动频率为0.51倍通道频率.并且其波动频率与前后静叶扰动强度无关.
参考文献
[1] | Storer J A;Cumpsty N A .An Approximate Analysis and Prediction Method for Tip Clearance Loss in Axial Compressors[R].ASME 93-GT-140,1993. |
[2] | T. V. Valkov;C. S. Tan .Effect of upstream rotor vortical disturbances on the time-averaged performance of axial compressor stators: part 2-- rotor tip vortex/streamwise vortex-stator blade interactions[J].Journal of turbomachinery,1999(3):387-397. |
[3] | Sirakov B T;Tan C S .Effects of Upstream Unsteady flow Conditions on Rotor Tip Leakage Flow[R].ASME GT-2002-30358,2002. |
[4] | Graf M B;Greitzer E M;Marble F E et al.Effects of Stator Pressure Field on Upstream Rotor Performance,1999[R].ASME 99-GT-99,1999. |
[5] | Mailach R;Sauer H;Vogeler K .The Periodical Interaction of the Tip Clearance Flow in the Blade Rows of Axial Compressor[R].ASME 2001-GT-0299,2001. |
[6] | Bae J;Breuer K S .Periodic Unsteadiness of Compressor Tip Clearance Votex[R].ASME 2004-GT-53015,2004. |
[7] | Chaoqun Nie;Gang Xu;Xiaobin Cheng;Jingyi Chen .Micro Air Injection and Its Unsteady Response in a Low-Speed Axial Compressor[J].Journal of turbomachinery,2002(4):572-579. |
[8] | Rai M M .Three-Dimensional Navier-Stokes Simulations of Turbine Rotor-Stator Interaction[J].AIAA Journal of Propulsion and Power,1989,5(03):306-311. |
[9] | Inoue M;Kuroumaru M .Structure of Tip Clearance Flow in an Isolated Axial Compressor Rotor[J].Journal of Turbomachinery,Transactions of the ASME,1989,111(02):250-256. |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%