航空工程进展2011，Vol.2Issue(3)：298-304,7.
叶型附面层分离流动控制技术研究进展
Advances in Flow Control Technology of Boundary Layer Separation on the Blade
周敏 1李航航 1唐侃平1
作者信息
- 1. 北京航空工程技术讲究中心,北京100076
- 折叠
摘要
Abstract
The flow control technology of boundary layer separation on the blade is applied to minish and control boundary layer separation and low energy flow on the blade suction surface to improve the efficiency and stability of compressor and turbine.The characteristic and effect mechanism of several kinds of flow control technology are presented in this paper,such as vortex generator jets,jet injection,boundary layer suction,boundary layer transition control and plasma assisted flow control.The domestic development of flow control technology of boundary layer separation on the blade is introduced.关键词
附面层分离/涡流发生器/射流注入/附面层抽吸/叶片附面层转捩控制/等离子体气动激励Key words
boundary layer separation/vortex generator jets/jet injection/boundary layer suction/boundary layer transition control/plasma assisted flow control引用本文复制引用
周敏,李航航,唐侃平..叶型附面层分离流动控制技术研究进展[J].航空工程进展,2011,2(3):298-304,7.
