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- W1997397789 abstract "The nonlinear aeroelastic characteristics of an aircraft wing with a control surface are investigated. A doublet-hybrid method is used for the calculation of subsonic unsteady aerodynamic forces and the minimum-state approximation is used for the approximation of aerodynamic forces. A free vibration analysis is performed using the finite element and the fictitious mass methods. The structural nonlinearity in the control surface hinge is represented by both free-play and a bilinear nonlinearity. These nonlinearities are linearized using the describing function method. From the nonlinear flutter analysis, various types of limit cycle oscillations and periodic motions are observed in a wide range of air speeds below the linear flutter boundary. The effects of structural nonlinearities on aeroelastic characteristics are investigated." @default.
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- W1997397789 date "2004-07-01" @default.
- W1997397789 modified "2023-10-18" @default.
- W1997397789 title "Effects of structural nonlinearity on subsonic aeroelastic characteristics of an aircraft wing with control surface" @default.
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- W1997397789 doi "https://doi.org/10.1016/j.jfluidstructs.2004.04.005" @default.
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