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• W2299385513 endingPage "1370" @default.
• W2299385513 startingPage "1359" @default.
• W2299385513 abstract "A method based on parametric reduced-order models to efficiently predict the transient response of aeroelastic systems with concentrated structural nonlinearities is presented. The approach approximates the nonlinear response in a piecewise-linear manner through time integration of sub-linear reduced-order models; these are parameterized with respect to the nonlinearity and are efficiently obtained by balanced truncation and interpolation. The procedure is applied to the optimization of a wing tip device for passive loads alleviation which features a nonlinear stiffness, showing the effectiveness and efficiency of the methodology." @default.
• W2299385513 created "2016-06-24" @default.
• W2299385513 creator A5006144112 @default.
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• W2299385513 date "2015-10-08" @default.
• W2299385513 modified "2023-10-16" @default.
• W2299385513 title "Parametric reduced-order model approach for simulation and optimization of aeroelastic systems with structural nonlinearities" @default.
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• W2299385513 doi "https://doi.org/10.1177/0954410015608888" @default.
• W2299385513 hasPublicationYear "2015" @default.
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