Numerical investigation of unsteady flow field in multi-stage compressor

被引：0
|
作者：
Wang, Yan-Gang [1 ]
Liu, Bo [1 ]
Guan, Ji-Wei [1 ]
Ma, Chang-You [1 ]
机构：
[1] National Laboratory of Airfoil and Cascade Aero-Dynamic, Northwestern Polytechnical Univ., Xi'an 710072, China
来源：
Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics | 2007年 / 28卷 / SUPPL. 1期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：125 / 128
相关论文
共 50 条
  • [21] Numerical investigation of unsteady flow field in a turbine stage with film-cooling
    2005, Science Press, Beijing, China (26):
  • [22] Experimental investigation on return passage of multi-stage centrifugal compressor
    Nakane, Ichirou
    Ariga, Ichirou
    Hayata, Takaaki
    Uchida, Masanori
    Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 1988, 54 (503): : 1677 - 1684
  • [23] Numerical analysis and optimization of the inlet stage of a multi-stage high pressure compressor
    National Key Laboratory on Aero-Engines, School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100083, China
    Hangkong Dongli Xuebao, 2007, 8 (1356-1364):
  • [24] IMPLEMENTATION OF A CENTRAL UPWIND SCHEME IN UNSTEADY COMPRESSIBLE FLOW SIMULATION OF MULTI-STAGE AXIAL-CENTRIFUGAL COMPRESSOR
    Jing, Zhenhao
    Neumeier, Yedidia
    Prasad, J. V. R.
    James, Darrell K.
    PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 13C, 2023,
  • [25] ACCOUNTING FOR CIRCUMFERENTIAL FLOW NONUNIFORMITY IN A MULTI-STAGE AXIAL COMPRESSOR
    Lou, Fangyuan
    Matthews, Douglas R.
    Kormanik, Nicholas J., III
    Key, Nicole L.
    PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2A, 2021,
  • [26] LARGE-SCALE DES ANALYSIS OF UNSTEADY FLOW FIELD IN A MULTI-STAGE AXIAL FLOW COMPRESSOR AT OFF-DESIGN CONDITION USING K COMPUTER
    Yamada, Kazutoyo
    Furukawa, Masato
    Nakakido, Satoshi
    Matsuoka, Akinori
    Nakayama, Kentaro
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 2C, 2015,
  • [27] Numerical investigation of the flow in a centrifugal compressor intermediate stage
    Li, Xue-Chen
    Xi, Guang
    Li, Xin-Wei
    Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2010, 31 (06): : 955 - 958
  • [28] Flow Field Measurement in Multi-stage Axial Compressor Stator by Using Multi-hole Pneumatic Probes
    Wang Zhiqiang
    Lu Bo
    Zhang Chenkai
    Hu Jun
    INTERNATIONAL JOURNAL OF TURBO & JET-ENGINES, 2017, 34 (01) : 81 - 94
  • [29] Multi-stage segmentation of optical flow field
    Choi, JG
    Kim, SD
    SIGNAL PROCESSING, 1996, 54 (02) : 109 - 118
  • [30] EXPERIMENTAL AND NUMERICAL STUDY OF RETURN CHANNEL FLOW INFLUENCE ON SURGE MARGIN OF A MULTI-STAGE CENTRIFUGAL COMPRESSOR
    Nishida, Yoshifumi
    Nishida, Hideo
    Kobayashi, Hiromi
    Nishioka, Takahiro
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 2C, 2015,
12345