Nonlinear modal interactions in composite thin-walled beam structures with simultaneous 1:2 internal and 1:1 external resonances

Nonlinear dynamic characteristics of a composite aircraft wing structure modeled by a geometrically nonlinear anisotropic thin-walled beam in the presence of simultaneous 1:2 internal and 1:1 external resonances are investigated. Some prominent non-classical effects such as of transverse shear strai...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
Veröffentlicht in:	Nonlinear dynamics 2016-10, Vol.86 (2), p.1381-1405
Hauptverfasser:	Wang, Xiao, Qin, Zhanming
Format:	Artikel
Sprache:	eng
Schlagworte:	Anisotropy Automotive Engineering Beams (structural) Classical Mechanics Computer simulation Control Dynamic characteristics Dynamical Systems Engineering Finite element method Galerkin method Galerkin methods Lay-up Mathematical models Mechanical Engineering Method of multiple scales Multiscale analysis Nonlinear dynamics Nonlinearity Original Paper Shear strain Stiffness Three dimensional models Twisting Vibration Wings (aircraft)
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Schreiben Sie den ersten Kommentar!