Aeroelastic stability of coupled flap-lag motion of hingeless helicopter blades at arbitrary advance ratios
- 1 April 1975
- journal article
- Published by Elsevier in Journal of Sound and Vibration
- Vol. 39 (4) , 409-428
- https://doi.org/10.1016/s0022-460x(75)80025-3
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
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- Aeroelastic Instabilities of Hingeless Helicopter BladesJournal of Aircraft, 1973
- Non-linear flap-lag dynamics of hingeless helicopter blades in hover and in forward flightJournal of Sound and Vibration, 1973
- Some Applications of the Method of Multiblade CoordinatesJournal of the American Helicopter Society, 1972
- Application of the Floquet Transition Matrix to Problems of Lifting Rotor StabilityJournal of the American Helicopter Society, 1971
- Investigations on the Effect of Blade Torsion on the Dynamics of the Flapping MotionJournal of the American Helicopter Society, 1970
- Dynamics of Rotors Operating at High Advance RatiosJournal of the American Helicopter Society, 1968
- Stability of a Flexible Helicopter Rotor Blade in Forward FlightJournal of the Aeronautical Sciences, 1956
- Stability of Rotor Blade Flapping Motion When the Hinges Are Tilted. Generalization of the "Rectangular Ripple" Method of SolutionJournal of the Aeronautical Sciences, 1947