The influence of trigger configurations and laminate lay-up on the failure mode of composite crush cylinders
Authors:
H. G. S. J. Thuis and V. H. Metz
Affiliation:
National Aerospace Laboratory, Voorsterveg 31, 8316 PR, Marknesse, The Netherlands
Abstract:
In this paper the results are presented of a test program on the energy absorption of composite cylinders loaded in compression. The influence of the laminate lay-up and of the trigger configuration were determined. Two different failure modes for the different laminates and triggers were observed: a splaying mode and a fragmentation mode. The splaying mode is more efficient in absorbing energy. The failure mode did not change during the crushing process.