Combined Flow Control of Positively Bowed Blade and Vortex Generator Jet on a Compressor Cascade

被引:1
|
作者
Li L. [1 ]
Song Y. [1 ]
Chen F. [1 ]
机构
[1] Department of Power Machinery and Engineering, Harbin Institute of Technology, Academy of Energy Science and Engineering, No. 92 Xidazhi Street, Nagang District, Harbin, Heilongjiang Province
来源
关键词
Combined flow control; Compressor cascade; Endwall vortex generator jet; Loss reduction; Positively bowed blade;
D O I
10.1515/tjj-2017-0011
中图分类号
学科分类号
摘要
A combined flow control method based on positively bowed blade and endwall vortex generator jet (VGJ) was performed to a compressor cascade under three kinds of inlet conditions. The results show that the endwall VGJ can further decrease the total losses in positively bowed cascades. At 0° incidence with zero inlet boundary layer, the separation type in the positively bowed blade is open, with the VGJ, the loss reduction is 2.7%. As the inlet boundary layer thickens at 0° incidence, the separation region increases with the separation type keeping unchanged, the loss reduction increasing to 11.73%. As the incidence rises to + 7° with zero inlet boundary layer, the separation type converts into closed and the flow separation is the severest in the three cases, with the VGJ, however, the loss reduction is just 7.4%, which means that the control effect of endwall VGJ not only depends on the size of separation region but also relies on the type of separation mode. If the separation type is open, as the size of separation region expands, the control effectiveness of endwall VGJ increases; if the separation type converts into closed with the further aggravation of flow field, that control effect will decrease. © 2020 De Gruyter. All rights reserved.
引用
收藏
页码:95 / 109
页数:14
相关论文
共 50 条
  • [1] Effects of vortex generator jet on the flow of bowed compressor cascades
    School of Energy Science and Engineering, Harbin Institute of Technology, Harbin
    150001, China
    Hangkong Dongli Xuebao, 11 (2658-2664):
  • [2] Flow control mechanisms of a combined approach using blade slot and vortex generator in compressor cascade
    Hu, Jiaguo
    Wang, Rugen
    Huang, Danqin
    AEROSPACE SCIENCE AND TECHNOLOGY, 2018, 78 : 320 - 331
  • [3] Flow Control on Bowed Compressor Cascades Using Vortex Generator Jet at Different Incidences
    Li, Longting
    Song, Yanping
    Chen, Fu
    Meng, Rui
    JOURNAL OF AEROSPACE ENGINEERING, 2017, 30 (05)
  • [4] EFFECTS OF VORTEX GENERATOR JET ON FLOW SEPARATIONS IN BOWED COMPRESSOR CASCADES
    Li, Longting
    Song, Yanping
    Chen, Fu
    Liu, Huaping
    ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 2A, 2015,
  • [5] Secondary flow control in high-turning compressor cascade using vortex generator jet
    Liu, Hua-Ping
    Chen, Huan-Long
    Li, De-Xiong
    Guo, Yu-Jie
    Cheng, Xiao-Qi
    Chen, Fu
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2015, 30 (04): : 838 - 845
  • [6] A parametric investigation of endwall vortex generator jet on the secondary flow control for a high turning compressor cascade
    Liu, Huaping
    Yu, Yongchuan
    Chen, Huanlong
    Yu, Menghan
    Zhang, Dongfei
    JOURNAL OF THERMAL SCIENCE AND TECHNOLOGY, 2017, 12 (01):
  • [7] EFFECT OF END-WALL VORTEX GENERATOR JET PARAMETERS ON FLOW CONTROL IN HIGH SUBSONIC COMPRESSOR CASCADE
    Chen, Cong
    Yu, Jianyang
    Chen, Fu
    PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 2A, 2018,
  • [8] 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
  • [9] Synthetic Separation Control Using Vortex Generator and Slot Jet in a High Load Compressor Cascade
    Hu, J.
    Wang, R.
    Wu, P.
    Li, F.
    JOURNAL OF APPLIED FLUID MECHANICS, 2017, 10 (05) : 1305 - 1318
  • [10] Vortex generator evaluation models and flow mechanisms for compressor cascade
    Ren, Xinyu
    Meng, Tongtong
    Zhu, Huiling
    Ji, Lucheng
    PHYSICS OF FLUIDS, 2024, 36 (11)