Active flutter suppression for two-dimensional airfoils
- 1 March 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Guidance, Control, and Dynamics
- Vol. 12 (2) , 188-194
- https://doi.org/10.2514/3.20390
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Reduced-Order Optimal Feedback Control Law Synthesis for Flutter SuppressionJournal of Guidance, Control, and Dynamics, 1982
- Control Law Synthesis for Flutter Suppression Using Linear Quadratic Gaussian TheoryJournal of Guidance and Control, 1981
- Modal Cost Analysis for Linear Matrix-Second-Order SystemsJournal of Dynamic Systems, Measurement, and Control, 1980
- An Elementary Explanation of the Flutter Mechanism with Active Feedback ControlsJournal of Aircraft, 1979
- Comparative Study Between Two Different Active Flutter Suppression SystemsJournal of Aircraft, 1978
- Active Flutter Control Using Generalized Unsteady Aerodynamic TheoryJournal of Guidance and Control, 1978