Morphing Wing Flight Control Via Postbuckled Precompressed Piezoelectric Actuators
- 1 July 2007
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 44 (4), 1060-1068
- https://doi.org/10.2514/1.21292
Abstract
No abstract availableKeywords
This publication has 23 references indexed in Scilit:
- Aerodynamic Performance of the Smart Wing Control EffectorsJournal of Intelligent Material Systems and Structures, 2004
- Development of High-rate, Adaptive Trailing Edge Control Surface for the Smart Wing Phase 2 Wind Tunnel ModelJournal of Intelligent Material Systems and Structures, 2004
- Overview of the DARPA Smart Wing ProjectJournal of Intelligent Material Systems and Structures, 2004
- Development of an SMA Actuator for In-flight Rotor Blade TrackingJournal of Intelligent Material Systems and Structures, 2004
- Defense Advanced Research Projects Agency – Smart Materials and Structures Demonstration Program OverviewJournal of Intelligent Material Systems and Structures, 2004
- Design and application of compliant mechanisms for morphing aircraft structuresPublished by SPIE-Intl Soc Optical Eng ,2003
- Design and testing of a 1/12th-scale solid state adaptive rotorSmart Materials and Structures, 1997
- Missile flight control using active flexspar actuatorsSmart Materials and Structures, 1996
- Active plate and wing research using EDAP elementsSmart Materials and Structures, 1992
- Effect of adaptive material properties on static aeroelastic controlPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992