Fundamental mechanisms of aeroelastic control with control surface and strain actuation
- 8 April 1991
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- The zeroes of controlled structures - Sensor/actuator attributes andstructural modellingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1991
- Typical section problems for structural control applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Digital-flutter-suppression-system investigations for the active flexible wing wind-tunnel modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Static aeroelastic behavior of an adaptive laminated piezoelectric composite wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- Induced strain actuation of isotropic and anisotropic platesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Aeroservoelastic wind-tunnel investigations using the active flexible wing model - Status and recent accomplishmentsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Aeroservoelastic modeling and applications using minimum-state approximations of the unsteady aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Field‐Forced Antiferroelectric‐to‐Ferroelectric Switching in Modified Lead Zirconate Titanate Stannate CeramicsJournal of the American Ceramic Society, 1989
- Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic ModelingJournal of Aircraft, 1982
- An Elementary Explanation of the Flutter Mechanism with Active Feedback ControlsJournal of Aircraft, 1979