Abstract
In this paper, an experiment is performed to investigate aeroelastic vibration control of a wing using regenerative piezoelectric actuators. Instead of the wing a plate with one pair of the piezoelectric actuator is used to study the effect of the vibrations. The model consists of the rectangular steel modelled in the cantilever configuration with the surface bonded with piezoelectric actuators. The regenerative actuators is used in the cantilever beam to harvest electrical power from the vibratory motion or provide an anti-vibratory control motion to cancel out the undesirable vibration in the cantilever beam.
Original language | English |
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Title of host publication | EUCASS 2013 - 5th European Conference for Aeronautics and Space Sciences |
Number of pages | 14 |
Publication status | Published - Jul 2013 |
Event | EUCASS 2013 - 5th European Conference for Aeronautics and Space Sciences - Munich, Germany Duration: 1 Jul 2013 → 5 Jul 2013 |
Conference
Conference | EUCASS 2013 - 5th European Conference for Aeronautics and Space Sciences |
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Country/Territory | Germany |
City | Munich |
Period | 1/07/13 → 5/07/13 |