Original paper
Damage in CFRPs due to low velocity impact at low temperature
Abstract
This work examines the response of carbon fibre-reinforced epoxy matrix (CFRP) laminates at low impact velocity and in low temperature conditions. Square specimens of carbon fibre/epoxy laminates with different stacking sequences (unidirectional, cross-ply, quasi-isotropic and woven laminates) were tested using a Drop Weight Tower device. The test temperature ranged from 20 down to −150 °C. After the impact tests, the damage extension was...
Paper Details
Title
Damage in CFRPs due to low velocity impact at low temperature
Published Date
Jan 1, 2005
Volume
36
Issue
1
Pages
41 - 50
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Notes
History