Effects of rotating inlet distortion on aerodynamic stability and stall inception of axial-flow compressor

被引：0
|
作者：
Zhang, Huan [1 ]
Hu, Jun [1 ]
Tu, Bao-Feng [1 ]
Wang, Zhi-Qiang [1 ]
Zhao, Yong [1 ]
机构：
[1] College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2008年 / 23卷 / 11期
关键词：
Aerodynamic stability;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：2095 / 2100
相关论文
共 50 条
  • [31] Role of blade passage flow structures in axial compressor rotating stall inception
    Hoying, D.A.
    Tan, C.S.
    Vo, Huu Duc
    Greitzer, E.M.
    Journal of Turbomachinery, 1999, 121 (04): : 735 - 742
  • [32] Effect of inlet radial distortion on aerodynamic stability in a multi-stage axial flow compressor
    Li, Jichao
    Du, Juan
    Liu, Yang
    Zhang, Hongwu
    Nie, Chaoqun
    AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 105
  • [33] Effects of rotating inlet distortion on multistage compressor stability
    Longley, JP
    Shin, HW
    Plumley, RE
    Silkowski, PD
    Day, IJ
    Greitzer, EM
    Tan, CS
    Wisler, DC
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1996, 118 (02): : 181 - 188
  • [34] Stall Warning Method Investigation and Application in an Axial-Flow Compressor with Circumferential Distortion
    Liu Y.
    Li J.-C.
    Du J.
    Zhang H.-W.
    Nie C.-Q.
    Tuijin Jishu/Journal of Propulsion Technology, 2020, 41 (09): : 1967 - 1974
  • [35] EFFECTS OF THE INLET BOUNDARY LAYER THICKNESS ON THE ROTATING STALL IN AN AXIAL COMPRESSOR
    Choi, Minsuk
    Baek, Je Hyun
    Oh, Seong Hwan
    Ki, Dock Jong
    PROCEEDINGS OF THE ASME FLUIDS ENGINEERING DIVISION SUMMER CONFERENCE, VOL 2, 2006, : 251 - 258
  • [36] EFFECTS OF THE INLET BOUNDARY LAYER THICKNESS ON ROTATING STALL IN AN AXIAL COMPRESSOR
    Choi, Minsuk
    Oh, Seong Hwan
    Ko, Han Young
    Baek, Je Hyun
    PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 6, PT A, 2008, : 497 - 507
  • [37] Effect of axial slot casing treatment on a counter-rotating axial-flow compressor aerodynamic performance and stability
    Guo, Yanchao
    Mao, Xiaochen
    Wang, Lei
    Gao, Limin
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2023, 237 (05) : 1185 - 1198
  • [38] Experimental Investigation of Circumferential Inlet Distortion on Partial Surge Type Stall Inception in Transonic Axial Compressor
    Yan, Jian-Dong
    Pan, Tian-Yu
    Wu, Wen-Qian
    Li, Qiu-Shi
    Tuijin Jishu/Journal of Propulsion Technology, 2023, 44 (01):
  • [39] Long-to-short length scale transition: A stall inception phenomenon in an axial compressor with inlet distortion
    Lin, Feng
    Li, Meilin
    Chen, Jingyi
    PROCEEDINGS OF THE ASME TURBO EXPO 2005, VOL 6, PTS A AND B, 2005, : 247 - 260
  • [40] Effects of Tip Leakage Flow on the Aerodynamic Performance and Stability of an Axial-Flow Transonic Compressor Stage
    Zhang, Botao
    Mao, Xiaochen
    Wu, Xiaoxiong
    Liu, Bo
    ENERGIES, 2021, 14 (14)
12345