Ítem
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Falcó Salcines, Olben
Mayugo Majó, Joan Andreu Lopes, Cláudio Saúl Gascons i Clarió, Narcís Costa i Balanzat, Josep |
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| agost 2014 | |
| Automated Fiber Placement is being extensively used in the production of major composite components for the aircraft industry. This technology enables the production of tow-steered panels, which have been proven to greatly improve the structural efficiency of composites by means of in-plane stiffness variation and load redistribution. However, traditional straight-fiber architectures are still preferred. One of the reasons behind this is related to the uncertainties, as a result of process-induced defects, in the mechanical performance of the laminates. This experimental work investigates the effect of the fiber angle discontinuities between different tow courses in a ply on the un-notched and open-hole tensile strength of the laminate. The influence of several manufacturing parameters are studied in detail. The results reveal that ’ply staggering’ and ’0% gap coverage’ is an effective combination in reducing the influence of defects in these laminates | |
| application/pdf | |
| 1359-835X | |
| http://hdl.handle.net/10256/9753 | |
| eng | |
| Elsevier | |
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Versió preprint del document publicat a: http://dx.doi.org/10.1016/j.compositesa.2014.03.022 Articles publicats (D-EMCI) |
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| © Composites Part A: Applied Science and Manufacturing, 2014, vol. 63, p. 21-31 | |
| Tots els drets reservats | |
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Materials compostos
Composite materials Fibres Fibers Indústria aeronàutica Aircraft industry |
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| Variable-stiffness composite panels: Defect tolerance under in-plane tensile loading | |
| info:eu-repo/semantics/article | |
| DUGiDocs |
