Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips

An edition of Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips (1995)

Aeroelasticity and structural optimization of composite helicopter rotor blades with swept tips

By K. A. Yuan

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Publish Date

1995

Publisher

National Aeronautics and Space Administration, Langley Research Center,National Technical Information Service, distributor

Language

eng

Pages

Description:

subjects: Dynamic response, Helicopters, Hamiltonian functions, Rotary wings, Aerodynamic loads, Mathematical models, Floquet theorem, Composite structures, Finite element method, Structural analysis, Aeroelasticity