Structural modeling of composite beams with induced-strain actuators
- 1 September 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (9), 1692-1701
- https://doi.org/10.2514/3.11832
Abstract
No abstract availableKeywords
This publication has 10 references indexed in Scilit:
- Structural response of composite beams and blades with elastic couplingsComposites Engineering, 1992
- Structural behavior of two-cell composite rotor blades with elastic couplingsAIAA Journal, 1992
- Experimental and theoretical analysis of composite I-beams with elastic couplingsAIAA Journal, 1991
- Induced strain actuation of isotropic and anisotropic platesAIAA Journal, 1991
- Analysis of piezoelectrically actuated beams using a layer-wise displacement theoryComputers & Structures, 1991
- Detailed Models of Piezoceramic Actuation of BeamsJournal of Intelligent Material Systems and Structures, 1990
- Effects of a piezo-actuator on a finitely deformed beam subjected togeneral loadingAIAA Journal, 1989
- Use of piezoelectric actuators as elements of intelligent structuresAIAA Journal, 1987
- Technical Notes: Hygrothermally Curvature Stable Laminates with Tension‐Torsion CouplingJournal of the American Helicopter Society, 1985
- Frequency Determination Techniques for Cantilevered Plates with Bending-Torsion Coupling.AIAA Journal, 1984