EFFECT OF PERIODIC ERRORS IN BLADE SETTING ON POTENTIAL INCOMPRESSIBLE-FLOW IN COMPRESSOR CASCADES

被引:0
|
作者
ELTAHER, RMM
SHAALAN, MRA
RASHED, MI
机构
关键词
D O I
10.1115/1.3448607
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:22 / 30
页数:9
相关论文
共 50 条
  • [1] EFFECT OF RANDOM ERRORS IN BLADE SETTING ON POTENTIAL INCOMPRESSIBLE-FLOW IN COMPRESSOR CASCADES
    ELTAHER, RMM
    SHAALAN, MRA
    RASHED, MI
    [J]. JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 1976, 98 (04): : 759 - 762
  • [2] A PARAMETRIC STUDY OF THE FLUTTER STABILITY OF 2-DIMENSIONAL TURBINE AND COMPRESSOR CASCADES IN INCOMPRESSIBLE-FLOW
    FORSCHING, H
    [J]. ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1989, 13 (06): : 351 - 364
  • [3] Effect of blade sweep on inlet flow in axial compressor cascades
    Chang Hao
    Zhu Fang
    Jin Donghai
    Gui Xingmin
    [J]. Chinese Journal of Aeronautics, 2015, (01) : 103 - 111
  • [4] Effect of blade sweep on inlet flow in axial compressor cascades
    Chang Hao
    Zhu Fang
    Jin Donghai
    Gui Xingmin
    [J]. Chinese Journal of Aeronautics, 2015, 28 (01) : 103 - 111
  • [5] Effect of blade sweep on inlet flow in axial compressor cascades
    Chang Hao
    Zhu Fang
    Jin Donghai
    Gui Xingmin
    [J]. CHINESE JOURNAL OF AERONAUTICS, 2015, 28 (01) : 103 - 111
  • [6] FLUTTER CONTROL OF INCOMPRESSIBLE-FLOW TURBOMACHINE BLADE ROWS BY SPLITTER BLADES
    CHIANG, HWD
    FLEETER, S
    [J]. JOURNAL DE PHYSIQUE III, 1994, 4 (04): : 783 - 804
  • [8] PREVENTION OF SEPARATION AND FLOW REVERSAL IN CORNERS OF COMPRESSOR BLADE CASCADES
    STRATFORD, BS
    [J]. AERONAUTICAL JOURNAL, 1973, 77 (749): : 249 - 256
  • [9] ON THE IMPLEMENTATION OF SYMMETRICAL AND ANTISYMMETRIC PERIODIC BOUNDARY-CONDITIONS FOR INCOMPRESSIBLE-FLOW
    SEGAL, G
    VUIK, K
    KASSELS, K
    [J]. INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 1994, 18 (12) : 1153 - 1165
  • [10] Effect of blade machining errors on compressor performance
    Cheng C.
    Wu B.
    Zheng H.
    Gao L.
    [J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2020, 41 (02):