Use of Multiblade Coordinates for Helicopter Flap-Lag Stability with Dynamic Inflow
- 1 February 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 17 (2) , 112-118
- https://doi.org/10.2514/3.57881
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
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- 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
- Terrain Following/Terrain Avoidance Flight with the AH‐56A VehicleJournal of the American Helicopter Society, 1971