Influence of structural damping, preconing offsets and large deflection on the flap-lag-torsional stability of a cantilevered rotor blade
- 27 May 1975
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Stability analysis of nonlinear autonomous systems - General theory and application to flutterPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Aeroelastic Instabilities of Hingeless Helicopter BladesJournal of Aircraft, 1973
- Non-linear flap-lag dynamics of hingeless helicopter blades in hover and in forward flightJournal of Sound and Vibration, 1973
- Stability of elastic bending and torsion of uniform cantilevered rotor blades in hoverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Exploration of Aeroelastic Stability Boundaries with a Soft-in-Plane Hingeless-Rotor ModelJournal of the American Helicopter Society, 1972