COMPARISON OF PERFORMANCE OF SUPERSONIC BLADING IN CASCADE AND IN COMPRESSOR ROTORS

被引:0
|
作者
MIKOLAJC.AA
JOHNSON, BV
机构
来源
MECHANICAL ENGINEERING | 1970年 / 92卷 / 08期
关键词
D O I
暂无
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:55 / &
相关论文
共 50 条
  • [41] A numerical study of shock wave/boundary layer interaction in a supersonic compressor cascade
    Dong Joo Song
    Hyun Chul Hwang
    Young In Kim
    [J]. KSME International Journal, 2001, 15 : 366 - 373
  • [42] Operation of centrifugal compressor as annular array of blading
    Bykov, G.A.
    Bykova, O.G.
    [J]. Khimicheskoe I Neftegazovoe Mashinostroenie, 2005, (10): : 17 - 20
  • [43] TURBULENT SKIN FRICTION ON AXIAL COMPRESSOR BLADING
    WALKER, GJ
    [J]. AIAA JOURNAL, 1990, 28 (07) : 1201 - 1202
  • [44] A numerical study of shock wave/boundary layer interaction in a supersonic compressor cascade
    Song, DJ
    Hwang, HC
    Kim, YI
    [J]. KSME INTERNATIONAL JOURNAL, 2001, 15 (03): : 366 - 373
  • [45] Impact of Surface Roughness on Compressor Cascade Performance
    Back, Seung Chul
    Sohn, June Hyuk
    Song, Seung Jin
    [J]. JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME, 2010, 132 (06): : 0645021 - 0645026
  • [46] A numerical study on a supersonic compressor cascade using k-ε turbulence closure
    Kim, SD
    Song, DJ
    Chung, IK
    [J]. HEAT TRANSFER 1998, VOL 6: GENERAL PAPERS, 1998, : 541 - 546
  • [47] Design methodology and predicted performance for a supersonic compressor stage
    Grosvenor, Allan D.
    Brown, Paul M.
    Lawlor, Shawn P.
    [J]. Proceedings of the ASME Turbo Expo 2006, Vol 6, Pts A and B, 2006, : 205 - 219
  • [48] Effects of passage parameters on performance of supersonic cascade
    Zhang, Shuying
    Zhou, Ling
    Ji, Lucheng
    [J]. Hangkong Dongli Xuebao/Journal of Aerospace Power, 2022, 37 (04): : 836 - 847
  • [49] DESIGN OF AXIAL COMPRESSOR BLADING BASED ON TESTS OF A LOW SPEED COMPRESSOR.
    McKenzie, A.B.
    [J]. Proceedings - Institution of Mechanical Engineers, 1980, 194 : 103 - 111
  • [50] PERFORMANCE OF 2 TRANSONIC AXIAL COMPRESSOR ROTORS INCORPORATING INLET COUNTERSWIRL
    LAW, CH
    WENNERSTROM, AJ
    [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1987, 109 (01): : 142 - 148