Random gust response statistics for coupled torsion-flapping rotor blade vibrations.
- 1 October 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 9 (10) , 726-729
- https://doi.org/10.2514/3.44334
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- An Advanced Stochastic Model for Threshold Crossing Studies of Rotor Blade VibrationsAIAA Journal, 1972
- Interpolation of aerodynamic damping of lifting rotors in forward flight from measured response varianceJournal of Sound and Vibration, 1971
- Stochastic properties of turbulence excited rotor blade vibrationsAIAA Journal, 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
- Rotary Wing Aircraft Design TrendsJournal of the American Helicopter Society, 1964