Flap-lag stability with dynamic inflow by the method of multiblade coordinatesfor rotor deflections in forward flight
- 4 April 1979
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Technical Notes: Application of Simplified Inflow Models to Rotorcraft Dynamic AnalysisJournal of the American Helicopter Society, 1976
- AN INVESTIGATION OF FLAP-LAG STABILITY OF WIND TURBINE ROTORS I N THE PRESENCE OF VELOCITY GRADIENTS AND HELICOPTER ROTORS I N FORWARD FLIGHTPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976
- Flap-Lag Stability of Helicopter Rotor Blades in Forward FlightJournal of the American Helicopter Society, 1975
- Some Approximations to the Flapping Stability of Helicopter RotorsJournal of the American Helicopter Society, 1974
- Random gust response statistics for coupled torsion-flapping rotor blade vibrations.Journal of Aircraft, 1972
- A general method with shaping filters to study random vibration statistics of lifting rotors with feedback controlsJournal of Sound and Vibration, 1972