Effects of blade leading edge lean and sweep on the aerodynamic performance of centrifugal impellers

被引:2
|
作者
Zhao, Huijing [1 ]
Wang, Zhiheng [1 ]
Tang, Yonghong [1 ]
Xi, Guang [1 ]
机构
[1] School of Energy and Power Engineering, Xi'an Jiaotong University, Xi'an,710049, China
关键词
D O I
10.7652/xjtuxb201511001
中图分类号
学科分类号
摘要
9
引用
收藏
页码:1 / 7
相关论文
共 50 条
  • [1] Effects of Compound Sweep and Lean on the Aerodynamic Performances of Transonic Centrifugal Impellers
    Zhao, Huijing
    Lu, Xiang
    Zhao, Guanhui
    Ma, Rui
    2019 5TH INTERNATIONAL CONFERENCE ON ENERGY MATERIALS AND ENVIRONMENT ENGINEERING, 2019, 295
  • [2] Effects of Leading-Edge Sweep Angle of Splitter Blade on Aerodynamic Performance of Micro-Centrifugal Compressor
    Fan, Ming-Xuan
    Liu, Jing-Yuan
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (09):
  • [3] AERODYNAMIC ANALYSIS IN LEAN BLADE EFFECTS IN CENTRIFUGAL COMPRESSOR
    Xu, Cheng
    Amano, R. S.
    Alkhalidi, A.
    PROCEEDINGS OF THE ASME INTERNATIONAL MECHANICAL ENGINEERING CONGRESS AND EXPOSITION, 2011, VOL 6, PTS A AND B, 2012, : 1355 - 1364
  • [4] Effect of the blade leading edge on the performance of a centrifugal compressor
    Chu, Lei-Zhe
    Du, Jian-Yi
    Huang, Dian-Gui
    Zhao, Xiao-Lu
    Xu, Jian-Zhong
    Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2008, 29 (05): : 767 - 769
  • [5] Effects of Cropped Blade Tip Leading Edge on Aerodynamic Performance of Transonic Compressor
    Qin, Li-Tao
    Zhang, Hai-Deng
    Zhou, Liu-Cheng
    He, Wei-Feng
    Wu, Yun
    Li, Ying-Hong
    Tuijin Jishu/Journal of Propulsion Technology, 2022, 43 (10):
  • [6] Mechanisms of Sweep on the Performance of Transonic Centrifugal Compressor Impellers
    He, Xiao
    Zheng, Xinqian
    APPLIED SCIENCES-BASEL, 2017, 7 (10):
  • [7] Effects of bionic volute tongue bioinspired by leading edge of owl wing on aerodynamic performance and noise of multi-blade centrifugal fan
    Liu, Xiaomin
    Li, Shuo
    Hsi-An Chiao Tung Ta Hsueh/Journal of Xi'an Jiaotong University, 2015, 49 (01): : 14 - 20
  • [8] AERODYNAMIC AND STRUCTURE CONSIDERATIONS IN CENTRIFUGAL COMPRESSOR DESIGN- BLADE LEAN EFFECTS
    Xu, C.
    Amano, R. S.
    PROCEEDINGS OF THE ASME TURBO EXPO 2012, VOL 8, PTS A-C, 2012, : 557 - 568
  • [9] Mechanisms of Lean on the Performance of Transonic Centrifugal Compressor Impellers
    He, Xiao
    Zheng, Xinqian
    JOURNAL OF PROPULSION AND POWER, 2016, 32 (05) : 1220 - 1229
  • [10] Leading-edge redesign of a turbomachinery blade and its effect on aerodynamic performance
    Zhang, Weihao
    Zou, Zhengping
    Ye, Jian
    APPLIED ENERGY, 2012, 93 : 655 - 667