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NASA NTRS ยท 19750048589

Large fracture toughness boron-epoxy composites

Abstract

The high tensile strengths of strong interfacial bonding may be combined with the large fracture toughness of weak interfacial bonding in brittle fiber/brittle matrix composites by intermittently coating the filaments before layup so as to have random alternate weak and strong regions. Appropriate coating materials enable Cook-Gordon Mode I interfacial debonding to take place, which produces very long pull-out lengths with an associated large contribution to toughness. Unidirectional boron-epoxy composites have been so made which have toughnesses greater than 200 kJ/sq m while retaining rule of mixtures tensile strengths. Similar trends have been observed for crossply layups.

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BibTeXRIS

Atkins, A. G.. 1975-05-01. Large fracture toughness boron-epoxy composites. https://ntrs.nasa.gov/citations/19750048589

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