Aeroelastic stability of composite hingeless rotor blades in hover—Part II: Results

Author:

Fulton M.V.,Hodges D.H.

Publisher

Elsevier BV

Subject

Computer Science Applications,Modelling and Simulation

Reference19 articles.

1. Investigations of hingeless rotor stability;Ormiston;Vertica,1983

2. Aeroelastic response and blade loads of a composite rotor in forward flight;Smith;Proceedings of the 33rd Structures, Structural Dynamics, and Materials Conference,1992

3. Aeroelastic stability analysis of a composite rotor blade;Hong;Journal of the American Helicopter Society,1985

4. Experimental-theoretical investigation of the vibration characteristics of rotating composite box-beams;Chandra;American Helicopter Society National Technical Specialists' Meeting on Rotorcraft Dynamics,1989

5. Large deflection static and dynamic finite element analysis of composite beams with arbitrary cross-sectional warping;Stemple;Proceedings of the 30th Structures, Structural Dynamics, and Materials Conference,1989

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