Effects of tip clearance grids on the simulations of three-dimensional flow fields in a low speed compressor rotor

被引:0
|
作者
National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics, Beijing 100083, China [1 ]
机构
来源
Hangkong Dongli Xuebao | 2006年 / 1卷 / 137-143期
关键词
Flow of fluids - Pressure - Rotors - Sensitivity analysis - Speed - Three dimensional;
D O I
暂无
中图分类号
学科分类号
摘要
The 3-D flow fields of a low-speed axial compressor rotor with a tip clearance were calculated. Compared with experimental results, effects of the tip grid-matching and the grid quality on numerical results were investigated. The result shows the requirement of the gird-matching between the tip clearance and the rotor passage for simulations of flow details in the tip clearance, and the sensitivity of the second-order difference scheme to the grid quality. In addition, it was revealed that the pressure rise characteristics did not exactly reflect the effect of grid numbers on numerical results.
引用
收藏
相关论文
共 50 条
  • [32] Numerical simulation of the effect of blade tip blowing on a low speed axial compressor tip clearance flow
    Dai, Li-Ping
    Zhang, Hui
    Kang, Shun
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2010, 25 (12): : 2643 - 2649
  • [33] Tip Flow Unsteadiness and Blade Row Interactions for a Low-Speed Compressor Rotor
    Lee, Daniel
    Orkwis, Paul D.
    Tsung, Fu-Lin
    Magnuszewski, William
    Noll, Christopher
    McNulty, G. Scott
    JOURNAL OF PROPULSION AND POWER, 2013, 29 (06) : 1346 - 1356
  • [34] Measurement of the three-dimensional tip region flow field in an axial compressor
    Stauter, R.C.
    Journal of Turbomachinery, 1993, 115 (03): : 468 - 476
  • [35] Investigation on unsteady tip clearance flow in a compressor by numerical simulations
    Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing 100080, China
    不详
    Kung Cheng Je Wu Li Hsueh Pao, 2006, 2 (229-231):
  • [36] Low-speed modeling design for tip flow field of compressor rotor blade
    School of Aeronautics and Astronautics, Shanghai Jiao Tong University, Shanghai
    200240, China
    不详
    110015, China
    Hangkong Dongli Xuebao, 1 (237-247):
  • [37] Three-dimensional turbulent flow field of axial compressor rotor passage
    Kung Cheng Je Wu Li Hsueh Pao, 3 (287-292):
  • [38] Electromagnetic Modeling of Three-Dimensional Flow in the Rotor of a Centrifugal Compressor.
    Ditman, A.O.
    Parfenov, B.A.
    Seleznev, K.P.
    Sherstyukov, V.A.
    Shkarbul', S.N.
    Energomashinostroenie, 1976, (09): : 7 - 9
  • [39] AERODYNAMIC PERFORMANCE OF LOW SPEED AXIAL FLOW COMPRESSOR ROTORS WITH SWEEP AND TIP CLEARANCE
    Ramakrishna, P. V.
    Govardhan, M.
    ENGINEERING APPLICATIONS OF COMPUTATIONAL FLUID MECHANICS, 2009, 3 (02) : 195 - 206
  • [40] Three-dimensional time-resolved measurements on rotor wake of low-speed axial compressor
    Wang, Si-Chen
    Li, Ji-Chao
    Lin, Feng
    Nie, Chao-Qun
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2014, 29 (12): : 2957 - 2964