Out-of-plane microbuckle growth is observed in a unidirectional carbon
fibre-epoxy matrix composite under compressive loading. Experimental
measurements of the overall kink-band width confirm that a growing mic
robuckle propagates in a crack-like manner rather than in a dislocatio
n-like manner. The microbuckle is modelled as a bridged Mode I crack w
ith compressive bridging tractions. A large scale bridging model with
a crack tip toughness and a constant bridging stress is successful in
correlating the length and width of a growing microbuckle with the rem
ote stress. Crown copyright (C) 1996