Semi-active flutter suppression for wing aileron with framework system

Wei Sun; Jian Sheng Wen; Hai Yan Hu

Semi-active flutter suppression for wing aileron with framework system

Wei Sun^*, Jian Sheng Wen, Hai Yan Hu

^*Corresponding author for this work

Nanjing University of Aeronautics and Astronautics

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

Abstract

A typical wing aileron system with a rudder driver framework is investigated. The magenetorheological (MR) damper is fixed on the framework instead of the aileron rotation axis. A set of four-degrees-of-freedom aeroelastic differential equations is developed and the on-off control algorithm is used to attenuate the vibration of the aileron. The numerical results show that the critical flutter speed is insensitive to the hysteresis of the MR damper. The higher apply voltage and the shorter control delay time can greatly increase the critical flutter speed. This configuration of the MR damper under the on-off control strategy can increase the critical flutter speed by 17% at least.

Original language	English
Pages (from-to)	422-426
Number of pages	5
Journal	Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics
Volume	36
Issue number	4
Publication status	Published - Aug 2004
Externally published	Yes

Keywords

Flutter suppression
Magenetorheological damper
On-off control
Wing

Cite this

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title = "Semi-active flutter suppression for wing aileron with framework system",

abstract = "A typical wing aileron system with a rudder driver framework is investigated. The magenetorheological (MR) damper is fixed on the framework instead of the aileron rotation axis. A set of four-degrees-of-freedom aeroelastic differential equations is developed and the on-off control algorithm is used to attenuate the vibration of the aileron. The numerical results show that the critical flutter speed is insensitive to the hysteresis of the MR damper. The higher apply voltage and the shorter control delay time can greatly increase the critical flutter speed. This configuration of the MR damper under the on-off control strategy can increase the critical flutter speed by 17% at least.",

keywords = "Flutter suppression, Magenetorheological damper, On-off control, Wing",

author = "Wei Sun and Wen, {Jian Sheng} and Hu, {Hai Yan}",

year = "2004",

month = aug,

language = "English",

volume = "36",

pages = "422--426",

journal = "Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics",

issn = "1005-2615",

publisher = "Nanjing University of Aeronautics an Astronautics",

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TY - JOUR

T1 - Semi-active flutter suppression for wing aileron with framework system

AU - Sun, Wei

AU - Wen, Jian Sheng

AU - Hu, Hai Yan

PY - 2004/8

Y1 - 2004/8

N2 - A typical wing aileron system with a rudder driver framework is investigated. The magenetorheological (MR) damper is fixed on the framework instead of the aileron rotation axis. A set of four-degrees-of-freedom aeroelastic differential equations is developed and the on-off control algorithm is used to attenuate the vibration of the aileron. The numerical results show that the critical flutter speed is insensitive to the hysteresis of the MR damper. The higher apply voltage and the shorter control delay time can greatly increase the critical flutter speed. This configuration of the MR damper under the on-off control strategy can increase the critical flutter speed by 17% at least.

AB - A typical wing aileron system with a rudder driver framework is investigated. The magenetorheological (MR) damper is fixed on the framework instead of the aileron rotation axis. A set of four-degrees-of-freedom aeroelastic differential equations is developed and the on-off control algorithm is used to attenuate the vibration of the aileron. The numerical results show that the critical flutter speed is insensitive to the hysteresis of the MR damper. The higher apply voltage and the shorter control delay time can greatly increase the critical flutter speed. This configuration of the MR damper under the on-off control strategy can increase the critical flutter speed by 17% at least.

KW - Flutter suppression

KW - Magenetorheological damper

KW - On-off control

KW - Wing

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M3 - Article

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SN - 1005-2615

VL - 36

SP - 422

EP - 426

JO - Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics

JF - Nanjing Hangkong Hangtian Daxue Xuebao/Journal of Nanjing University of Aeronautics and Astronautics

IS - 4

ER -

Semi-active flutter suppression for wing aileron with framework system

Abstract

Keywords

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