Effect of Impact Position on Repaired Composite Laminates Subjected to Multi-Impacts
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DOI: 10.3390/ma15228039
Abstract: Because the certification of aircraft structures requires significant costs and time-consuming experimental tests, all the studies carried out are strong contributions to the applicability of repairs based on adhesively bonded fibre composite patches. In this… read more here.
Keywords: effect; position repaired; impact; effect impact ... See more keywords