Stability and Control of Hingeless Rotor Helicopter Ground Resonance
- 1 June 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (6) , 333-339
- https://doi.org/10.2514/3.59254
Abstract
No abstract availableKeywords
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- The Influence of Blade Flapping Restraint on the Dynamic Stability of Low Disk Loading Propeller‐RotorsJournal of the American Helicopter Society, 1967
- A summary of hingeless-rotor structural loads and dynamics researchJournal of Sound and Vibration, 1966
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