STABILITY OF HINGELESS ROTOR BLADES I N HOVER WITH PITCH-LINK FLEXIBILITY
- 5 May 1976
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Influence of structural damping, preconing offsets and large deflection on the flap-lag-torsional stability of a cantilevered rotor bladePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Some Conclusions Regarding the Aeroelastic Stability of Hingeless Helicopter Blades in Hover and in Forward FlightJournal of the American Helicopter Society, 1973
- Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in HoverJournal of the American Helicopter Society, 1972
- A Quadratically Convergent Newton-Like Method Based Upon Gaussian EliminationSIAM Journal on Numerical Analysis, 1969