Beschreibung:
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<jats:title content-type="abstract-heading">Purpose</jats:title>
<jats:p> – T-sections of carbon fibre-reinforced composites are prone to delamination because they lack reinforcement through their thicknesses. The purpose of this paper is to present the structural response of cost-effective laminated T-sections when subjected to various types of loads and impacts. </jats:p>
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<jats:title content-type="abstract-heading">Design/methodology/approach</jats:title>
<jats:p> – The core of the automated manufactured beams is analysed. Pull-off, flange tension, and flange bending were tested for specimens extracted from an I-beam. The failure processes for all of the specimens were investigated in detail, leading to the statistical evaluation of the failure modes. </jats:p>
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<jats:title content-type="abstract-heading">Findings</jats:title>
<jats:p> – A correlation is apparent between the impact damage energy and certain fracture patterns. These results can be used to assess damage tolerance when designing stiffeners, beams, and various complex structures. The increase in strength by 25 per cent was measured for the advanced stitching located in the web section for the flange tension test. </jats:p>
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<jats:title content-type="abstract-heading">Originality/value</jats:title>
<jats:p> – The resistance displayed by the T-sections toward impact damage was studied experimentally, as the literature describing this topic is limited. The prevalence of one fracture mode for higher impact energies shows a possible advantage of the cost-effective preforms for the damage tolerant philosophy.</jats:p>
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