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• W2058462021 abstract "Composite T-stiffener structures are widely used structural elements in weight sensitive structural, aerospace and marine applications for the purpose of weight reduction. A study on the process-induced deformation of composite T-stiffener structures is presented in this paper. The deformation was calculated numerically by Finite Element Analysis (FEA), and the resulting displacements show that the deformation can be represented by a single angular displacement: the spring-in of the skin. A parametric study was conducted by Design of Experiments (DOE) and FEA to investigate the influence of design parameters on the spring-in of the skin. It is shown that the spring-in of the skin increases with the radius and the bonding length, and decreases with the fiber volume fraction." @default.
• W2058462021 created "2016-06-24" @default.
• W2058462021 creator A5082147189 @default.
• W2058462021 date "2010-06-01" @default.
• W2058462021 modified "2023-10-16" @default.
• W2058462021 title "Process-induced deformation of composite T-stiffener structures" @default.
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• W2058462021 doi "https://doi.org/10.1016/j.compstruct.2009.11.026" @default.
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