Structural and mechanism design of an active trailing-edge flap blade-Reference-Cited by-同舟云学术

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Structural and mechanism design of an active trailing-edge flap blade

Published:2013-09 Issue:9 Volume:27 Page:2605-2617
ISSN:1738-494X
Container-title:Journal of Mechanical Science and Technology
language:en
Short-container-title:J Mech Sci Technol

Author:

Lee Jae Hwan,Natarajan Balakumaran,Eun Won Jong,Viswamurthy S. R.,Park Jae-Sang,Kim Taesong,Shin Sang Joon

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://link.springer.com/content/pdf/10.1007/s12206-013-0704-8.pdf

Reference29 articles.

1. J. T. Pearson, R. M. Goodall and I. Lyndon, Active control of helicopter vibration, Comput. Control. Eng. J., 5(6) (1994) 277–284.

2. J. K. Shim and S. Na, Active vibration control of flexible cantilever beam using Piezo actuator and filtered-X LMS algorithm, KSME Intl. J., 12(4) (1998) 665–671.

3. J. Lee, J. Kim and C.-C. Cheong, Piezoelectric smart structures for noise reduction in a cabin, KSME Intl. J., 13(6) (1999) 451–458.

4. J. K. Shim and S. Na, Modeling and vibration feedback control of rotating tapered composite thin-walled blade, KSME Intl. J., 17(3) (2003) 380–390.

5. J.-Y. Jeon, Passive vibration damping enhancement of piezoelectric shunt damping system using optimization approach, J. Mech. Sci. Technol., 23(5) (2009) 1435–1445.

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