Abstract
The aim of this work is to find optimum shapes of holes in shear panels made of carbon/epoxy composite materials. The study is restricted to non-buckling shear panels, and a simplified fracture criterion is applied. Starting with a baseline square shear panel with a circular hole, the optimization results in a larger non-circular hole that gives the same maximum stress level in the laminate. Optimum shaped holes are determined for four different laminate configurations, the differences between the shapes being small.
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References
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© 1988 Kluwer Academic Publisher
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Bäcklund, J., Isby, R. (1988). Shape Optimization of Holes in Composite Shear Panels. In: Rozvany, G.I.N., Karihaloo, B.L. (eds) Structural Optimization. Springer, Dordrecht. https://doi.org/10.1007/978-94-009-1413-1_2
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DOI: https://doi.org/10.1007/978-94-009-1413-1_2
Publisher Name: Springer, Dordrecht
Print ISBN: 978-94-010-7132-1
Online ISBN: 978-94-009-1413-1
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