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- W13341856 abstract "This paper is focused on the free vibration analysis of aircraft wing models through 1D higherorder models. Refined 1D finite elements were obtained by exploiting the Carrera Unified Formulation (CUF); the 1D models proposed adopt polynomial expansions of the displacement field above the structure cross-section. Two classes of CUF 1D models were developed, the Taylor Expansion models (TE) exploit N-order Taylor-like polynomials, whereas the Lagrange Expansion models (LE) are based on Lagrange polynomials defined on a number of subdomains (L-element) of the cross-section. The order and the type of the cross-section expansion can be arbitrarily chosen since CUF models are hierarchical, that is, the order and the class of the model are input of the analysis. This fundamental capability is obtained by exploiting the fundamental nucleus (FN) of the problem matrices. FN arrays are formally independent of the order and the class of the model. Therefore, stiffness, mass and loading arrays are obtained with no need of ad hoc formulations. CUF 1D models provide 3D-like accuracies with low computational costs for a wide variety of structural configurations, including thin walled structures and composites. In this paper, CUF 1D models were adopted to analyze complex aircraft wings. The typical components of such structures (panels, ribs and stiffeners) were modeled by means of 1D models. The free vibration analysis was conducted and results were compared with solid models by commercial codes. Results highlighted the enhanced capabilities of CUF 1D in terms of implementation ease, high accuracy and low computational costs." @default.
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- W13341856 date "2012-01-01" @default.
- W13341856 modified "2023-09-27" @default.
- W13341856 title "Free vibration analysis of complex wing structures by refined one-dimensional formulations" @default.
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