Stability of Hingeless Rotor Blades in Hover with Pitch-Link Flexibility
- 1 April 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 15 (4), 476-482
- https://doi.org/10.2514/3.60652
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Influence of Modeling and Blade Parameters on the Aeroelastic Stability of a Cantilevered RotorAIAA Journal, 1977
- 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