Stability of elastic bending and torsion of uniform cantilevered rotor blades in hover
- 20 March 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Technical Notes: The Effects of Second Order Blade Bending on the Angle of Attack of Hingeless Rotor BladesJournal of the American Helicopter Society, 1973
- Aeroelastic instabilities of hingeless helicopter bladesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- A Theory of Rotor Blade Motion Stability in Powered FlightJournal of the American Helicopter Society, 1964