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
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