Aeroelastic analysis of rotor systems using trailing edge flaps
Author:
Publisher
Elsevier BV
Subject
Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics
Reference19 articles.
1. The nonlinear behavior of elastic slender straight beams undergoing small strains and moderate rotations;Rosen;ASME Journal of Applied Mechanics,1979
2. D.H. Hodges, E.H. Dowell, Nonlinear equations of motion for elastic bending and torsion of twisted non-uniform rotor blades, NASA TN D-7818, 1974.
3. Aeroelastic response and stability analysis of composite rotor blades in forward flight;Jeon;Composites: Part B,2001
4. Aeroelastic analysis of bearingless rotors using large deflection beam theory;Lim;AIAA Journal,2007
5. Helicopter vibration reduction using structural optimization with aeroelastic/multidisciplinary constraints—a survey;Friedmann;Journal of Aircraft,1991
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