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
来源
Proceedings of the ASME Turbo Expo 2005, Vol 6, Pts A and B | 2005年
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
  • [41] Control of endwall secondary flow in a compressor cascade with dielectric barrier discharge plasma actuation
    Li Gang
    Xu YanJi
    Lin Bin
    Zhu JunQiang
    Nie ChaoQun
    Ma HongWei
    Wang ZhaoFeng
    SCIENCE IN CHINA SERIES E-TECHNOLOGICAL SCIENCES, 2009, 52 (12): : 3715 - 3721
  • [42] Control mechanism of vortex-generator jet on turbulent separation in a highly loaded compressor cascade
    Cao, Zhiyuan
    Song, Cheng
    Guo, Wei
    Wang, Chuxuan
    Gao, Xi
    Liu, Bo
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART C-JOURNAL OF MECHANICAL ENGINEERING SCIENCE, 2023, 237 (21) : 4957 - 4978
  • [43] Mechanisms of oscillating suction in controlling the tip leakage flow in a high-load compressor cascade
    Zhang, Botao
    Mao, Xiaochen
    Liu, Bo
    Wang, Hejian
    Yang, Zonghao
    Chen, Qidong
    AEROSPACE SCIENCE AND TECHNOLOGY, 2023, 133
  • [44] Analysis of Compressor Cascade Deviation and Surrogate Model Construction Based on Retained Lift
    Hu, Haojie
    Jin, Donghai
    JOURNAL OF THERMAL SCIENCE, 2025, 34 (02) : 567 - 578
  • [45] Effect of unilateral blade tip fillet structure on blade tip clearance flow of compressor cascade
    Gao L.
    Wang H.
    Zhao L.
    Li Y.
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2020, 35 (09): : 1927 - 1935
  • [46] Investigation of transition flow on suction surface of highly loaded compressor cascade controlled by plasma actuator
    Zhang, Yining
    Yu, Jianyang
    Chen, Fu
    Song, Yanping
    INTERNATIONAL JOURNAL OF HEAT AND FLUID FLOW, 2024, 105
  • [47] Calibration of Spalart-Allmaras model for simulation of corner flow separation in linear compressor cascade
    Matsui, Kotaro
    Perez, Ethan
    Kelly, Ryan
    Tani, Naoki
    Jemcov, Aleksandar
    JOURNAL OF THE GLOBAL POWER AND PROPULSION SOCIETY, 2021,
  • [48] Simulation Analysis Of Compressor Flow Field In Vehicle Turbocharger
    Lei, Rujing
    2019 11TH INTERNATIONAL CONFERENCE ON MEASURING TECHNOLOGY AND MECHATRONICS AUTOMATION (ICMTMA 2019), 2019, : 199 - 203
  • [49] Effectiveness of Blade Surface Roughness on 3D Corner Separation and Loss in Compressor Cascade
    Liu K.
    Chu W.-L.
    Zhang H.-G.
    Chen X.-Y.
    Li J.-G.
    Li L.-P.
    Tuijin Jishu/Journal of Propulsion Technology, 2019, 40 (03): : 504 - 514
  • [50] NUMERICAL AND EXPERIMENTAL STUDY ON FLOW LOSS REDUCTION EFFECT OF MICRO-TEXTURED SURFACE ON COMPRESSOR CASCADE
    Wang, Liyue
    Wang, Cong
    Sun, Gang
    Feng, Jinzhang
    PROCEEDINGS OF ASME TURBO EXPO 2024: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2024, VOL 12A, 2024,