Modeling of a Helicopter Fuselage Panel with Active Vibration Control
Author:
Affiliation:
1. Department of Mechatronics Engineering, KTO Karatay University, Turkey
2. Department of Mechanical Engineering, KTO Karatay University, Turkey
Publisher
ACM Press
Reference14 articles.
1. Kozek M, Benatzky C, Schirrer A, Stribersky A. Vibration damping of a flexible car body structure using piezo-stack actuators. Control Engineering Practice. 2011; 19: 298--310.
2. Karagülle H, Malgaca L, ve Oktem HF. Analysis of active vibration control in smart structures by ANSYS. Smart Materials and Structures. 2004; 13(4): 661--667.
3. Jalili N. Piezoelectric-Based Vibration Control: From Macro to Micro/Nano Scale Systems. Springer; 2009.
4. Bales G, Glaese RM, Anderson EH, Shaw L. Active Damping and Vibration Control for Aircraft Fin and Appendage Structures. 44th AIAA Aerospace Sciences Meeting And Exhibit, 2006:653.
5. Mendoza J, Chevva K, Sun F, Blanc A, Kim SB. Active Vibration Control for Helicopter Interior Noise Reduction Using Power Minimization. NASA/CR--2014-218147. United Technologies Research Center East Hartford:2014.
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