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- W2365005769 abstract "A finite element model of the aeroelastic helicopter rotor in transitional flight is built from the energy variation principle,the blade response to the transient rotor speed is especially considered.The elemental aerodynamic forces are figured out according to the rotor element theory in more complex inflow model.All components of wind velocity and pitch angle and roll angle of the main rotor shaft are considered in the air speed calculation.The transient responses of the blade in flap,lag and pitch displacement are simulated using a frigate wake flow.The model here can be widely used in the vibration analysis,noise estimation or fault diagnosis of the helicopter rotor." @default.
- W2365005769 created "2016-06-24" @default.
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- W2365005769 date "2007-01-01" @default.
- W2365005769 modified "2023-09-25" @default.
- W2365005769 title "Research on Rotor Aeroelastic FEM Model in Transitional Flight" @default.
- W2365005769 hasPublicationYear "2007" @default.
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