Aeroelastic stability of complete rotors with application to a teetering rotor in forward flight

Author:

Shamie J.,Friedmann P.

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Acoustics and Ultrasonics,Condensed Matter Physics

Reference23 articles.

1. Dynamic non-linear elastic stability of helicopter rotor blades in hover and forward flight;Friedmann;NASA-CR-114485,1972

2. Stability of elastic bending and torsion of uniform cantilevered rotor blades in hover;Hodges,1973

3. Influence of modeling and blade parameters on the aeroelastic stability of a cantilevered rotor;Friedmann;American Institute of Aeronautics and Astronautics Journal,1977

4. Aeroelastic stability of periodic systems with application to rotor blade flutter;Friedmann;American Institute of Aeronautics and Astronautics Journal,1974

5. Aeroelastic stability of coupled flap-lag motion of hingeless helicopter blades at arbitrary advance ratios;Friedmann;Journal of Sound and Vibration,1975

Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Performance Advantages and Resonance Analysis of a Variable Speed Rotor Using Geometrically Exact Beam Formulations;Journal of the American Helicopter Society;2022-10-01

2. Transient response analysis of gimballed tiltrotors during engage and disengage operations;39th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference and Exhibit;1998-04-20

3. Aeroelastic stability and response analysis of large horizontal-axis wind turbines;Journal of Wind Engineering and Industrial Aerodynamics;1980-05

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