Access the full text.
Sign up today, get DeepDyve free for 14 days.
Loading next page...
/lp/sage/anisotropic-actuation-with-piezoelectric-fiber-composites-FlkKK90DXH
References (9)
-
S. Ehlers, T. Weisshaar (1992)
Effect of adaptive material properties on static aeroelastic control -
D. Skinner, R. Newnham, L. Cross (1978)
Flexible composite transducersMaterials Research Bulletin, 13
-
N. Hagood, R. Kindel, K. Ghandi, P. Gaudenzi (1993)
Improving transverse actuation of piezoceramics using interdigitated surface electrodes, 1917
-
W. Smith, Bertram, Auld (1991)
Modeling 1-3 composite piezoelectrics: thickness-mode oscillationsIEEE Transactions on Ultrasonics, Ferroelectrics and Frequency Control, 38
-
E. Crawley, K. Lazarus (1989)
Induced strain actuation of isotropic and anisotropic platesAIAA Journal, 29
-
R. Barrett (1993)
Modeling techniques and design principles of a low-aspect-ratio active aeroservoelastic wing, 1917
-
E. Crawley, E. Anderson (1989)
Detailed Models of Piezoceramic Actuation of BeamsJournal of Intelligent Material Systems and Structures, 1
-
N. Hagood, A. Bent (1993)
DEVELOPMENT OF PIEZOELECTRIC FIBER COMPOSITES FOR STRUCTURAL ACTUATION -
N. Hagood, W. Chung, A. Flotow (1990)
Modelling of Piezoelectric Actuator Dynamics for Active Structural ControlJournal of Intelligent Material Systems and Structures, 1
- Publisher
- SAGE
- Copyright
- Copyright © by SAGE Publications
- ISSN
- 1045-389X
- eISSN
- 1530-8138
- DOI
- 10.1177/1045389X9500600305
- Publisher site
- See Article on Publisher Site
Abstract
An investigation was made into the field of planar structural actuation with anisotropic active materials. The mechanisms for creating anisotropic actuators were discussed, and the impact of anisotropy was shown at the individual lamina level and at the laminated structure level. Models for laminated structures were developed using an augmented Classical Laminated Plate Theory incorporating induced stress terms to accommodate anisotropic actuator materials. A twistextension coupled laminate was used to exemplify how twist can be directly induced into isotropic host structures using anisotropic actuation. Four anisotropic actuators with different material anisotropies were compared using this example. Finally, a laminate incorporating piezoelectric fiber composite actuators was manufactured and tested. Excellent agreement was found between the predicted and experimental response.
Journal
Journal of Intelligent Material Systems and Structures – SAGE
Published: May 1, 1995