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

Research output: Contribution to journal › Article › peer-review

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.

Original language	English
Pages (from-to)	107-110
Number of pages	4
Journal	Chinese Journal of Sensors and Actuators
Volume	20
Issue number	1
State	Published - Jan 2007

Keywords

Boundary layer
Flow control
Micro actuator arrays

Cite this

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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.",

keywords = "Boundary layer, Flow control, Micro actuator arrays",

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AU - Yao, Zhan Chao

AU - Yuan, Wei Zheng

AU - Dang, Jin Jun

AU - Ma, Bing He

AU - Jiang, Cheng Yu

PY - 2007/1

Y1 - 2007/1

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

UR - https://www.scopus.com/pages/publications/34248364833

M3 - 文章

AN - SCOPUS:34248364833

SN - 1004-1699

VL - 20

SP - 107

EP - 110

JO - Chinese Journal of Sensors and Actuators

JF - Chinese Journal of Sensors and Actuators

IS - 1

ER -

Aerodynamic research of actuator in flow control

Abstract

Keywords

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