The inherent brittleness of continuous unidirectional fibre reinforced composites is a major drawback to their otherwise outstanding mechanical performance. This paper exploits composites with overlapped discontinuities at the ply level to create a significantly non-linear response, due to progressive interlaminar damage under tensile loading. Two distinct configurations were manufactured with the same carbon/epoxy system and tested under quasi-static tension, showing that varying the thickness and length of the overlapping ply blocks resulted in significantly different mechanical responses and failure. modes. A previously developed generalised shear-lag model was successfully used to optimise the overlap configuration, and accurately predicted the response in both strength- and toughness-dominated cases. This work demonstrates that unidirectional composites with well-designed discontinuities at the ply level can provide a significantly non-linear response with clear warning before failure, while retaining similar stiffness and up to 50% of the strength of their continuous counterparts. (C) 2014 The Authors. Published by Elsevier Ltd.
机构:Univ Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA
Cleveland, Tyler
;
Ciccu, Marco
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机构:Univ Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA
Ciccu, Marco
;
Stickler, Patrick
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机构:
Boeing Co, Boeing Commercial Airplanes, Boeing Technol Integrat 787, Everett, WA USAUniv Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA
Stickler, Patrick
;
DeOto, Luciano
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h-index: 0
机构:
Automobili Lamborghini SpA, Adv Composites Dev Ctr, I-40019 St Agata Bolognese, ItalyUniv Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA
机构:Univ Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA
Cleveland, Tyler
;
Ciccu, Marco
论文数: 0引用数: 0
h-index: 0
机构:Univ Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA
Ciccu, Marco
;
Stickler, Patrick
论文数: 0引用数: 0
h-index: 0
机构:
Boeing Co, Boeing Commercial Airplanes, Boeing Technol Integrat 787, Everett, WA USAUniv Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA
Stickler, Patrick
;
DeOto, Luciano
论文数: 0引用数: 0
h-index: 0
机构:
Automobili Lamborghini SpA, Adv Composites Dev Ctr, I-40019 St Agata Bolognese, ItalyUniv Washington, Dept Aeronaut & Astronaut, Automobili Lamborghini Adv Composite Struct Lab, Seattle, WA 98195 USA