Vibration reduction in helicopter rotors using an active control surface located on the blade
- 13 April 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Application of Higher Harmonic Control to Rotors Operating at High Speed and ThrustJournal of the American Helicopter Society, 1990
- Analytic simulation of higher harmonic control using a new aeroelastic modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- A Unified Approach to the Optimal Design of Adaptive and Gain Scheduled Controllers to Achieve Minimum Helicopter Rotor VibrationJournal of the American Helicopter Society, 1983
- Effect of gaps on the loading distribution of planar lifting surfaces.AIAA Journal, 1968