Syed Mohamed Ali, Jaffar and Khan, Md. Raisuddin and Hamid, Md.Tarique (2011) Structural analysis of an active beam. In: Advances in aircraft structure. IIUM Press, Kuala Lumpur, pp. 125-130. ISBN 978-967-418-148-2
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Abstract
An adaptive beam model of anisotropically actuated beam is formulated to determine the displacement and twist actuation capabilities of anisotropic piezoelectric actuators as related to the potential application for the helicopter blade control. The chosen beam has been modeled in ANSYS. Some existing results on piezoeletric actuators with different combinations and lay-ups were verified.
Item Type: | Book Chapter |
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Additional Information: | 4625/20254 |
Uncontrolled Keywords: | Smart structures, piezoelectric, helicopter blades, active control |
Subjects: | T Technology > TL Motor vehicles. Aeronautics. Astronautics |
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button): | Kulliyyah of Engineering > Department of Mechatronics Engineering |
Depositing User: | Dr. Md. Raisuddin Khan |
Date Deposited: | 14 Jul 2012 06:49 |
Last Modified: | 14 Jul 2012 06:49 |
URI: | http://irep.iium.edu.my/id/eprint/20254 |
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