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.
Keep this discovery
Explore connections, maps & timelines
Atkins, A. G.. 1975-05-01. Large fracture toughness boron-epoxy composites. https://ntrs.nasa.gov/citations/19750048589
Cite the original work for its findings. Save a collection to share your selection of sources.