Aerodynamic performance optimization on S2 analysis code of multi-stage axial compressor

被引:0
|
作者
Guo, Yi [1 ]
Du, Gang [1 ]
Chen, Jiang [1 ]
Yin, Hong-Shun [2 ]
机构
[1] School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
[2] China Gas Turbine Establishment, Aviation Industry Corporation of China, Chengdu 610500, China
来源
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:953 / 960
相关论文
共 50 条
  • [12] Sensors for aerodynamic instabilities applied to a multi-stage compressor
    Preute, R
    Eikelmann, J
    Servaty, S
    TECHNISCHES MESSEN, 1997, 64 (06): : 238 - 246
  • [13] Aerodynamic instability evolution of a multi-stage combined compressor
    Jiaan LI
    Xinqian ZHENG
    Chinese Journal of Aeronautics, 2025, 38 (01) : 291 - 301
  • [14] Aerodynamic instability evolution of a multi-stage combined compressor
    Li, Jiaan
    Zheng, Xinqian
    CHINESE JOURNAL OF AERONAUTICS, 2025, 38 (01)
  • [15] Aerodynamic instability evolution of a multi-stage combined compressor
    ZHENG, Xinqian (zhengxq@tsinghua.edu.cn), 1600, Elsevier B.V. (38):
  • [16] AERODYNAMIC AND ROTORDYNAMIC PERFORMANCE OF A MULTI-STAGE CENTRIFUGAL COMPRESSOR WITH HIGH HUB IMPELLERS
    Srinivasan, Anand
    David, Tim
    Silva, Daniel
    Rajagopalan, Vinayaka
    Kurz, Rainer
    PROCEEDINGS OF ASME TURBO EXPO 2023: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2023, VOL 9, 2023,
  • [17] Performance Prediction and IGV-stator Adjustment Optimization of a Multi-stage Axial-flow Compressor
    Zhang, Xia-Wen
    Ju, Ya-Ping
    Zhang, Chu-Hua
    Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2020, 41 (06): : 1418 - 1424
  • [18] Axial flow, multi-stage turbine and compressor models
    Tournier, Jean-Michel
    El-Genk, Mohamed S.
    ENERGY CONVERSION AND MANAGEMENT, 2010, 51 (01) : 16 - 29
  • [19] NUMERICAL INVESTIGATION ON THE INFLUENCE OF WET COMPRESSION AERODYNAMIC PERFORMANCE OF MULTI-STAGE TRANSONIC COMPRESSOR
    Zhu, Zihuan
    Ming, Lele
    Zhang, Xinze
    Wu, Yadong
    Ouyang, Hua
    PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 12A, 2024,
  • [20] 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):