Dynamic stability of a rotor blade using finite element analysis
- 9 April 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Non-linear dynamic analysis of rotors by finite element methodJournal of Sound and Vibration, 1980
- Application of the Finite Element Method to Rotary‐Wing AeroelasticityJournal of the American Helicopter Society, 1980
- Vibration of a rotating beam with tip massJournal of Sound and Vibration, 1979
- Vibration and Response of Nonuniform Rotating Beams with DiscontinuitiesJournal of the American Helicopter Society, 1979
- Rotor blade vibrations by the galerkin finite element methodJournal of Sound and Vibration, 1975
- Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in HoverJournal of the American Helicopter Society, 1972