Research on the stability enhancement mechanism of multi-parameter interaction of casing treatment in an axial compressor rotor

被引:4
|
作者
Chi, Zhidong [1 ]
Chu, Wuli [1 ]
Zhang, Ziyun [1 ]
Zhang, Haoguang [1 ]
机构
[1] Northwestern Polytech Univ, Sch Power & Energy, 127 Youyi Rd,Xi, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
axial compressor; casing treatment; response surface method; multi-parameter interaction; tip leakage flow; INJECTION;
D O I
10.1177/09544100211063079
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The research on geometric parameters of casing treatment (CT) has always been a hot topic, yet the multi-parameter interaction is rarely studied. In order to gain better knowledge of the interaction mechanism of geometric parameters of CT, the experimental and numerical study based on the response surface method has been carried out in an axial compressor rotor. First of all, the statistical analysis based on the database of experimental and numerical results is presented to summarize the influence law of varied parameters on the stability enhancement. It was found that axial overlap, open area ratio, and their interaction had the most significant influence on the stability enhancement of CT. Subsequently, the interaction between axial overlap and open area ratio was analyzed by visualization flow field in details, which provided a deeper insight into stability enhancement mechanism of CT. It indicated that the mass flow and momentum dominated by injection and the suction effect played a key role for extending stability. With smaller open area ratio, it was difficult for the slots to manipulate and control the tip leakage flow or secondary tip leakage flow, resulting in the weak effect of CT on compressor performance. Finally, the underlying flow physics in the tip region and dominant region of CT has also been discussed to penetrate the essential reason of multi-parameter interaction.
引用
收藏
页码:2405 / 2419
页数:15
相关论文
共 50 条
  • [21] Numerical study on the stability enhancement mechanism of self-recirculating casing treatment in a counter-rotating axial-flow compressor
    Guo, Yanchao
    Mao, Xiaochen
    Gao, Limin
    Yu, Yibo
    ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 2022, 16 (01) : 1111 - 1130
  • [22] Mechanism of Stability Enhancement with Shallow Reversed Slot-Type Casing Treatment in a Transonic Compressor
    Chi, Z. D.
    Chu, W. L.
    Zhang, H. G.
    JOURNAL OF APPLIED FLUID MECHANICS, 2021, 14 (06) : 1691 - 1704
  • [23] Effect of wire mesh casing treatment on axial compressor performance and stability
    Ming ZHANG
    Jiaming ZHANG
    Jiahao HU
    Xu DONG
    Dakun SUN
    Xiaofeng SUN
    Chinese Journal of Aeronautics , 2024, (03) : 60 - 76
  • [24] Effect of wire mesh casing treatment on axial compressor performance and stability
    Zhang, Ming
    Zhang, Jiaming
    Hu, Jiahao
    Dong, Xu
    Sun, Dakun
    Sun, Xiaofeng
    CHINESE JOURNAL OF AERONAUTICS, 2024, 37 (03) : 60 - 76
  • [25] Mechanism of influences of axial positions of axial skewed slot casing treatment on a compressor performance
    Zhang, Hao-Guang
    Chu, Wu-Li
    Wu, Yan-Hui
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2011, 26 (01): : 92 - 98
  • [26] Failure mechanism of casing treatment in improving stability of a highly loaded two-stage axial compressor
    Wang Wei
    Lu Jin-ling
    Luo Xing-qi
    Huang Rui
    Chu Wu-li
    AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 105
  • [27] Effects of Circumferential Coverage Ratio and Axial Position of Injector on Axial Compressor Stability Enhancement with Self-Recirculating Casing Treatment
    Wang G.
    Chu W.-L.
    Chi Z.-D.
    Chen X.-Y.
    Zhang H.-G.
    Tuijin Jishu/Journal of Propulsion Technology, 2020, 41 (06): : 1237 - 1249
  • [28] Study of Axial Matching of Rotor/Stator for a High-Loaded Axial Flow Compressor with Casing Treatment
    Wang W.
    Li X.
    Lu J.-L.
    Luo X.-Q.
    Chu W.-L.
    Tuijin Jishu/Journal of Propulsion Technology, 2019, 40 (07): : 1505 - 1513
  • [29] Application of adaptive treatment casing in multi-stage axial compressor
    Yin C.
    Yin Y.
    He X.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2019, 34 (06): : 1373 - 1379
  • [30] Mechanism of Combined Effect of Blade Sweeping and Casing Treatment in Transonic Compressor Rotor
    Chi, Zhi-Dong
    Chu, Wu-Li
    Wang, Guang
    Zhang, Zi-Yun
    Zhang, Hao-Guang
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (04):