EFFECT OF THE INLET VELOCITY PROFILE IN THE 3-DIMENSIONAL FLOW IN A REAR AXIAL COMPRESSOR STAGE

被引：6
|
作者：
CYRUS, V
机构：
来源：
JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME | 1988年 / 110卷 / 04期
关键词：
D O I：
10.1115/1.3262216
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
引用
收藏
页码：434 / 440
页数：7
相关论文
共 50 条
  • [1] Effect of the inlet velocity profile in the three-dimensional flow in a rear axial compressor stage
    Cyrus, V.
    Journal of Turbomachinery, 1988, 110 (04): : 434 - 440
  • [2] MEASUREMENT OF 3-DIMENSIONAL FLOW FIELD BEHIND AN AXIAL COMPRESSOR STAGE
    HIRSCH, C
    KOOL, P
    JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1977, 99 (02): : 168 - 180
  • [3] 3-DIMENSIONAL FLOW PHENOMENA IN A TRANSONIC, HIGH-THROUGHFLOW, AXIAL-FLOW COMPRESSOR STAGE
    COPENHAVER, WW
    HAH, C
    PUTERBAUGH, SL
    CUMPSTY, NA
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1993, 115 (02): : 240 - 248
  • [4] Simulating the flow field in a rear stage of a multistage axial flow compressor
    Li, Y.G.
    Tourlidakis, A.
    International Journal of Turbo and Jet Engines, 2002, 19 (1-2): : 1 - 11
  • [5] Simulating the flow field in a rear stage of a multistage axial flow compressor
    Li, YG
    Tourlidakis, A
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2002, 19 (1-2) : 1 - 11
  • [6] PROPAGATION OF INLET FLOW DISTORTIONS THROUGH AN AXIAL COMPRESSOR STAGE
    COLPIN, J
    JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME, 1979, 101 (01): : 116 - 124
  • [7] A repeating stage model in flow predictions of axial flow compressor rear stages
    Li, YG
    Tourlidakis, A
    Elder, RL
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2001, 18 (03) : 219 - 230
  • [8] 3-DIMENSIONAL FLOW IN DEEP ROTATING STALL CELLS OF AN AXIAL COMPRESSOR
    MATHIOUDAKIS, K
    BREUGELMANS, FAE
    JOURNAL OF PROPULSION AND POWER, 1988, 4 (03) : 263 - 269
  • [9] 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
  • [10] CALCULATION OF 3-DIMENSIONAL SUPERSONIC-FLOW IN AN AXIAL COMPRESSOR BY A METHOD OF CHARACTERISTICS
    MARTINON, J
    RECHERCHE AEROSPATIALE, 1978, (04): : 161 - 174
12345