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Modelling piezoelectric actuation during structural flutter

conference contribution
posted on 2024-10-31, 09:23 authored by Mohammed Hariri, Sabu JohnSabu John, Pavel TrivailoPavel Trivailo
Aeroelasticity is a major concern in structural control. It results from the interaction between the air-stream and the structure. Wing flutter is a well known problem of the aero-elasticity. It occurs when the two lowest system eigenvalues (plunge and pitch motion) coalesce at a certain air speed known as the flutter speed. The increasing use of active material induced-strain actuation such as piezoelectric materials in the suppression of structural vibrations has seen its extension to wing flutter control.

History

Start page

1

End page

11

Total pages

11

Outlet

Proceedings of the ASME 2009 Conference on Smart Materials, Adaptive Structures and Intelligent Systems (SMASIS 2009)

Editors

C. S. Lynch and D. Brei

Name of conference

ASME 2009 Conference on Smart Materials, Adaptive Structures and Intelligent Systems (SMASIS 2009)

Publisher

AMSE (American Society of Mechanical Engineers)

Place published

Ashland, USA

Start date

2009-09-21

End date

2009-09-23

Language

English

Copyright

© 2009 ASME

Former Identifier

2006017568

Esploro creation date

2020-06-22

Fedora creation date

2010-04-09

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