Experimental investigation of the performance of a supersonic compressor cascade

被引：2
|
作者：
Tweedt, D.L.
Schreiber, H.A.
Starken, H.
机构：
来源：
Journal of Turbomachinery | 1988年 / 110卷 / 04期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
15
引用
收藏
页码：456 / 466
相关论文
共 50 条
  • [1] EXPERIMENTAL INVESTIGATION OF THE PERFORMANCE OF A SUPERSONIC COMPRESSOR CASCADE
    TWEEDT, DL
    SCHREIBER, HA
    STARKEN, H
    JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1988, 110 (04): : 456 - 466
  • [2] Aerodynamic Design Method and Experimental Investigation of a High-Load Supersonic Compressor Cascade
    Yan, Tingsong
    Yan, Peigang
    Liang, Zhuoming
    Chen, Huanlong
    JOURNAL OF THERMAL SCIENCE, 2024, 33 (06) : 2075 - 2088
  • [3] Aerodynamic Design Method and Experimental Investigation of a High-Load Supersonic Compressor Cascade
    YAN Tingsong
    YAN Peigang
    LIANG Zhuoming
    CHEN Huanlong
    Journal of Thermal Science, 2024, 33 (06) : 2075 - 2088
  • [4] Effect of supersonic compressor cascade throat on flow pattern and cascade performance
    Jiang X.
    Qiu M.
    Fan Z.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2017, 38 (03):
  • [5] COMPARISON OF PERFORMANCE OF SUPERSONIC BLADING IN CASCADE AND IN COMPRESSOR ROTORS
    MIKOLAJC.AA
    MORRIS, AL
    JOHNSON, BV
    JOURNAL OF ENGINEERING FOR POWER, 1971, 93 (01): : 42 - &
  • [6] COMPARISON OF PERFORMANCE OF SUPERSONIC BLADING IN CASCADE AND IN COMPRESSOR ROTORS
    MIKOLAJC.AA
    JOHNSON, BV
    MECHANICAL ENGINEERING, 1970, 92 (08) : 55 - &
  • [7] An experimental investigation of the effects of upstream probe disturbance on compressor cascade performance
    Xiang, Honghui
    Ge, Ning
    Hou, Minjie
    Gao, Jie
    Yang, Rongfei
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2017, 231 (07) : 1248 - 1257
  • [8] SUPERSONIC CASCADE TUNNEL USED TO EVALUATE COMPRESSOR BLADE PERFORMANCE
    STUBNER, AW
    CASE, LF
    BLAKE, TR
    JOURNAL OF ENGINEERING FOR POWER, 1966, 88 (02): : 153 - &
  • [9] SUPERSONIC CASCADE TUNNEL USED TO EVALUATE COMPRESSOR BLADE PERFORMANCE
    STUBNER, AW
    BLAKE, TR
    CASE, LF
    MECHANICAL ENGINEERING, 1966, 88 (01) : 68 - &
  • [10] EXPERIMENTAL INVESTIGATION OF EFFECTS OF LEADING-EDGE TUBERCLES ON COMPRESSOR CASCADE PERFORMANCE
    Keerthi, M. C.
    Kushari, Abhijit
    De, Ashoke
    Kumar, Arun
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2014, VOL 2A, 2014,
12345