Active plate and missile wing development using directionally attached piezoelectric elements
- 1 March 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 32 (3), 601-609
- https://doi.org/10.2514/3.12027
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- A study on the feasibility of using adaptive structures in the attenuation of vibration characteristics of rotary wingsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Induced strain actuation of isotropic and anisotropic platesAIAA Journal, 1991
- Active control of torsional vibration using piezoceramic sensors andactuatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Detailed models of piezoceramic actuation of beamsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Use of piezoelectric actuators as elements of intelligent structuresAIAA Journal, 1987
- Optimal vibration control by the use of piezoceramic sensors and actuatorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987