Analysis of flow mechanism in 2-D compressor cascade with splitter

被引:0
|
作者
Li Haipeng [1 ]
Liu Houxing [1 ]
Zou Zhengping [1 ]
机构
[1] Beijing Univ Aeronaut & Astronaut, Natl Lab Aircraft Engine, Beijing 100083, Peoples R China
关键词
splitter; compressor cascade; flow field; 2-D;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
Through numeric simulation of flow in different turning angle cascades with different splitters, the flow mechanism in 2-D compressor cascade with splitter is particularly analyzed in this paper. The study result shows that the splitter can influence the flow field in cascade intensively; the positive attack angle on the splitter leading is an important cause that brings about cascade loss growth. If the splitter chord is short, the presence of splitter has little influence on the cascade inlet flow field, but has intense influence on the outlet flow field. by the modification of splitter, the pressure distribution of cascade can be greatly changed, the separation flow in the cascade can be restrained effectively, and the performance of splitter cascade can be effectively improved. On the condition of maintaining a high mass flux, the presence of splitter can greatly raise the loading of cascade.
引用
收藏
页码:125 / 134
页数:10
相关论文
共 50 条
  • [1] Numerical simulation analysis of leakage flow in compressor cascade with splitter
    Li, Haipeng
    Liu, Huoxing
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2007, 33 (01): : 22 - 26
  • [2] Accurate 2-D Modelling of Transonic Compressor Cascade Aerodynamics
    Piovesan, Tommaso
    Magrini, Andrea
    Benini, Ernesto
    AEROSPACE, 2019, 6 (05)
  • [3] Numerical analysis of cavitating flow through a 2-D decelerating cascade
    Shin, BR
    Iga, Y
    Ikohagi, T
    COMPUTATIONAL FLUID DYNAMICS 2000, 2001, : 651 - 656
  • [4] FLOW ANALYSIS AND UNCERTAINTY QUANTIFICATION OF A 2D COMPRESSOR CASCADE WITH DIRTY BLADES
    Qin, Ruihong
    Ju, Yaping
    Wang, Yazhou
    Zhang, Chuhua
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2016, VOL 2C, 2016,
  • [5] Numerical analysis of 2-D unsteady cavitating flow around hydrofoils in cascade
    Iga, Yuka
    Nohmi, Motohiko
    Goto, Akira
    Shin, Byeong Rog
    Ikohagi, Toshiaki
    Nippon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B, 2002, 68 (666): : 368 - 374
  • [6] RIBLETS IN TURBULENT FLOW REGIMES OF 2-D COMPRESSOR BLADES
    Klumpp, Stephan
    Meinke, Matthias
    Schroeder, Wolfgang
    Feldhaus, Bjoern
    Klocke, Fritz
    PROCEEDINGS OF ASME TURBO EXPO 2009, VOL 7, PTS A AND B, 2009, : 81 - 90
  • [7] Unsteady 2-D flow field characteristics for perforated plates with a splitter
    Yaragal, SC
    WIND AND STRUCTURES, 2004, 7 (05) : 317 - 332
  • [8] Flow performance analysis in an axial compressor rotor with splitter
    Yan, Ming
    Chen, Mao-Zhang
    Tuijin Jishu/Journal of Propulsion Technology, 2002, 23 (04): : 280 - 282
  • [9] Pressure based method for 2-D transonic cascade flow
    Liu, Jubin
    Chen, Xidi
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2000, 18 (01): : 105 - 110
  • [10] PERFORMANCE EVALUATION OF LEADING EDGE TUBERCLES APPLIED TO THE BLADES IN A 2-D COMPRESSOR CASCADE
    Sidhu, Satpreet S.
    Asghar, Asad
    Allan, William D. E.
    PROCEEDINGS OF ASME TURBO EXPO 2021: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, VOL 2A, 2021,