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- W178776119 abstract "Nonlinear aeroelastic analyses of composite wing with flap are performed considering free-play and dynamic stiffness of actuator. Doublet-Hybrid method is used for the calculation of subsonic unsteady aerodynamic forces. Free-play is modeled as a bilinear spring and is linearized by using the describing function method. Dynamic stiffness is obtained from governing equation of gear system and the aeroelastic analyses were performed according to ply-angle of laminate and material. The linear and nonlinear flutter analysis results show that the flutter characteristics are significantly dependent on the free-play and dynamic stiffness. from the nonlinear flutter analysis, various types of limit cycle oscillations are observed in a range of air speeds below or above the linear divergent flutter boundary." @default.
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- W178776119 date "2007-01-01" @default.
- W178776119 modified "2023-09-27" @default.
- W178776119 title "Nonlinear Aeroelastic Analyses of Composite Wing with Flap" @default.
- W178776119 hasPublicationYear "2007" @default.
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