Structural modeling of manufacture-induced gaps and overlaps by high-order unified finite elements
Alberto Racionero Sánchez-Majanodownload PDF
Abstract. Variable stiffness composites present additional tailoring capabilities if compared to classical straight fiber composites. However, the fabrication of these advanced composites leads inevitably to the presence of manufacturing signatures such as gaps and overlaps, which alter the mechanical behavior of the laminated components. In this work, the fundamental frequency of variable stiffness laminates with the presence of gaps and overlaps is studied. The Defect Layer Method is considered for modeling the defects, while the Carrera Unified Formulation is employed to derive the governing equations which will be solved by the Finite Element Method.
Variable Angle Tow Composites, Defect Modeling, Gaps and Overlaps, Unified Formulation
Published online 9/1/2023, 8 pages
Copyright © 2023 by the author(s)
Published under license by Materials Research Forum LLC., Millersville PA, USA
Citation: Alberto Racionero Sánchez-Majano, Structural modeling of manufacture-induced gaps and overlaps by high-order unified finite elements, Materials Research Proceedings, Vol. 33, pp 301-308, 2023
The article was published as article 44 of the book Aerospace Science and Engineering
Content from this work may be used under the terms of the Creative Commons Attribution 3.0 license. Any further distribution of this work must maintain attribution to the author(s) and the title of the work, journal citation and DOI.
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