Examination of the flap-lag stability of rigid articulated rotor blades
- 1 December 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 16 (12) , 876-884
- https://doi.org/10.2514/3.44643
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
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- Linear Flap-Lag Dynamics of Hingeless Helicopter Rotor Blades in HoverJournal of the American Helicopter Society, 1972
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- Aeroelastic Instability of Torsionally Rigid Helicopter BladesJournal of the American Helicopter Society, 1967
- Recent Studies of the Pitch‐Lag Instabilities of Articulated RotorsJournal of the American Helicopter Society, 1961
- Pitch‐Lag Instability of Helicopter RotorsJournal of the American Helicopter Society, 1958