AN ACTUATOR DISC ANALYSIS OF INLET DISTORTION AND ROTATING STALL IN AXIAL FLOW TURBOMACHINES

被引：12
|
作者：
YEH, H
机构：
来源：
JOURNAL OF THE AEROSPACE SCIENCES | 1959年 / 26卷 / 11期
关键词：
D O I：
10.2514/8.8286
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：739 / 753
页数：15
相关论文
共 50 条
  • [21] Stability analysis for rotating stall dynamics in axial flow compressors
    Guoxiang Gu
    Andrew Sparks
    Calin Belta
    Circuits, Systems and Signal Processing, 1999, 18 : 331 - 350
  • [22] Influence of inlet distortion on the stall character of a low speed axial compressor
    Jiang, Hua-Bing
    Lu, Ya-Jun
    Yuan, Wei
    Li, Qiu-Shi
    Hou, An-Ping
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2008, 23 (02): : 355 - 360
  • [23] The role of tip leakage flow in triggering rotating stall of a low speed compressor under inlet distortion
    Jingxuan Zhang
    Feng Lin
    Jingyi Chen
    Chaoqun Nie
    Journal of Thermal Science, 2009, 18 : 33 - 39
  • [24] The Role of Tip Leakage Flow in Triggering Rotating Stall of a Low Speed Compressor under Inlet Distortion
    Zhang, Jingxuan
    Lin, Feng
    Chen, Jingyi
    Nie, Chaoqun
    JOURNAL OF THERMAL SCIENCE, 2009, 18 (01) : 33 - 39
  • [25] Visualisation of rotating stall in an axial flow fan
    Fike, Matej
    Bombek, Gorazd
    Hribersek, Matjaz
    Hribernik, Ales
    EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2014, 53 : 269 - 276
  • [26] Rotating stall control for axial flow compressors
    Belta, C
    Gu, GX
    Sparks, A
    Banda, S
    AUTOMATICA, 2001, 37 (06) : 921 - 931
  • [27] Rotating stall control for axial flow compressors
    Belta, C
    Gu, GX
    Sparks, A
    Banda, S
    PROCEEDINGS OF THE 37TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-4, 1998, : 2557 - 2562
  • [28] Partial tip air injection to extend the stall margin in an axial flow compressor with circumferential inlet distortion
    Li, Jichao
    Liu, Yang
    Liu, Jingyuan
    Peng, Feng
    Zhang, Hongwu
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 144
  • [29] The Role of Tip Leakage Flow in Triggering Rotating Stall of a Low Speed Compressor under Inlet Distortion
    Jingxuan Zhang~1
    Journal of Thermal Science, 2009, 18 (01) : 33 - 39
  • [30] 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
12345