Separation Control by Slot Jet in a Critically Loaded Compressor Cascade

被引:12
|
作者
Hu, Jiaguo [1 ,2 ]
Wang, Rugen [1 ]
Wu, Peigen [1 ]
He, Chen [1 ]
机构
[1] Air Force Engn Univ, Sch Aeronaut & Astronaut Engn, Xian 710038, Shaanxi, Peoples R China
[2] Beihang Univ, Sch Energy & Power Engn, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
critically loaded compressor cascade; flow control; slot; jet; vortices model; ACTIVE FLOW-CONTROL;
D O I
10.1515/tjj-2016-0044
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Separation in compressor cascade triggers flow loss and instability. This paper presents a passive flow control method by introducing a slot into the blade. The slot induces self-adapted jet, while the jet flow is used to suppress cascade's separation. To study the flow control effect, experiments were conducted and flow field details were given by validated numerical simulations. The results show that a well-designed slot carries adequate jet airflow from pressure side (PS) to suction side (SS) due to the great pressure fall between the two sides. The jet airflow delays suction side separation within specific incidence angles, so the performance of cascade achieves considerable improvements. It enables to be concluded that the slot carries jet flow to SS separation zone, and then the self-adapted jet flow re-energizes low momentum fluid and suppresses vortices in the separation which are negative to the cascade flow.
引用
收藏
页码:229 / 239
页数:11
相关论文
共 50 条
  • [21] Flow separation control on a highly loaded compressor cascade using endwall synthetic jets
    Qin, Yong
    Song, Yanping
    Wang, Ruoyu
    Liu, Huaping
    Chen, Fu
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (11) : 2059 - 2075
  • [22] Numerical Study of Dual Sweeping Jet Actuators for Corner Separation Control in Compressor Cascade
    Meng, Qinghe
    Du, Xin
    Chen, Shaowen
    Wang, Songtao
    JOURNAL OF THERMAL SCIENCE, 2021, 30 (01) : 201 - 209
  • [23] Experimental investigation of adaptive Coanda jet control for performance improvement of a highly loaded compressor cascade
    Zhang, Jian
    Zhang, Min
    Du, Juan
    Nie, Chaoqun
    PHYSICS OF FLUIDS, 2025, 37 (04)
  • [24] Corner Separation Control by Boundary Layer Suction Applied to a Highly Loaded Axial Compressor Cascade
    Liu, Yangwei
    Sun, Jinjing
    Lu, Lipeng
    ENERGIES, 2014, 7 (12): : 7994 - 8007
  • [25] Numerical Investigation of Flow Separation Control on a Highly Loaded Compressor Cascade by Plasma Aerodynamic Actuation
    ZHAO Xiaohu LI Yinghong WU Yun ZHU Tao LI Yiwen Science and Technology on Plasma Dynamics Laboratory Air Force Engineering University Xian China
    Chinese Journal of Aeronautics, 2012, 25 (03) : 349 - 360
  • [26] Effect of combined boundary layer suction on the separation control in a highly loaded transonic compressor cascade
    Li, Bai
    Mu, Guangyuan
    Luo, Lei
    Du, Wei
    Zhou, Xun
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART A-JOURNAL OF POWER AND ENERGY, 2024, 238 (02) : 217 - 231
  • [28] Boundary layer separation control on a highly-loaded, low-solidity compressor cascade
    Zhou Yang
    Liu Huo-xing
    Zou Zheng-ping
    Ye Jian
    JOURNAL OF THERMAL SCIENCE, 2010, 19 (02) : 97 - 104
  • [29] Boundary layer separation control on a highly-loaded, low-solidity compressor cascade
    Yang Zhou
    Huo-xing Liu
    Zheng-ping Zou
    Jian Ye
    Journal of Thermal Science, 2010, 19 : 97 - 104