Aeroelastic stability of a soft-inplane gimballed tiltrotor model in hover
- 11 June 2001
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Design, Analysis, and Test of a Composite Tailored Tiltrotor WingJournal of the American Helicopter Society, 2000
- Tiltrotor Vibration Reduction Through Higher Harmonic ControlJournal of the American Helicopter Society, 1998