Aerodynamic research of actuator in flow control

Zhan Chao Yao; Wei Zheng Yuan; Jin Jun Dang; Bing He Ma; Cheng Yu Jiang

Aerodynamic research of actuator in flow control

Zhan Chao Yao, Wei Zheng Yuan, Jin Jun Dang, Bing He Ma, Cheng Yu Jiang

Northwestern Polytechnical University Xian

科研成果: 期刊稿件 › 文章 › 同行评审

摘要

Based on the technology of micro-electro-mechanical systems (MEMS), a balloon actuator was developed. The micro actuators arrays were put on a delta wing. CFD (computational fluid dynamics) simulations and wind tunnel experiments carried out about micro balloon actuator's influence on boundary layer separation eddy. The actuators can change the leading-edge vortices. And consequently, micro actuators on the proper position can provide sufficient rolling moments for flow control and change the dynamics quality of aircraft.

源语言	英语
页（从-至）	107-110
页数	4
期刊	Chinese Journal of Sensors and Actuators
卷	20
期	1
出版状态	已出版 - 1月 2007

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title = "Aerodynamic research of actuator in flow control",

abstract = "Based on the technology of micro-electro-mechanical systems (MEMS), a balloon actuator was developed. The micro actuators arrays were put on a delta wing. CFD (computational fluid dynamics) simulations and wind tunnel experiments carried out about micro balloon actuator's influence on boundary layer separation eddy. The actuators can change the leading-edge vortices. And consequently, micro actuators on the proper position can provide sufficient rolling moments for flow control and change the dynamics quality of aircraft.",

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AU - Yao, Zhan Chao

AU - Yuan, Wei Zheng

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AU - Ma, Bing He

AU - Jiang, Cheng Yu

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N2 - Based on the technology of micro-electro-mechanical systems (MEMS), a balloon actuator was developed. The micro actuators arrays were put on a delta wing. CFD (computational fluid dynamics) simulations and wind tunnel experiments carried out about micro balloon actuator's influence on boundary layer separation eddy. The actuators can change the leading-edge vortices. And consequently, micro actuators on the proper position can provide sufficient rolling moments for flow control and change the dynamics quality of aircraft.

AB - Based on the technology of micro-electro-mechanical systems (MEMS), a balloon actuator was developed. The micro actuators arrays were put on a delta wing. CFD (computational fluid dynamics) simulations and wind tunnel experiments carried out about micro balloon actuator's influence on boundary layer separation eddy. The actuators can change the leading-edge vortices. And consequently, micro actuators on the proper position can provide sufficient rolling moments for flow control and change the dynamics quality of aircraft.

KW - Boundary layer

KW - Flow control

KW - Micro actuator arrays

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Aerodynamic research of actuator in flow control

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