Effects Of Stacking Sequence On Compression Response Testing Of Carbon Fibre And Hybrids: Fibrous-Glass/Carbon/Kevlar/ Epoxy Composite Plates
Abstract
This paper is concerned with evaluation of
failure mechanisms under compression loading in
unidirectional composites and the in-plane dimensional
of fibre-reinforced laminated composites under
compression loads. (0/0/0/0/0/0)s oriented cross-ply
Fibrous-Glass/Carbon/Kevlar/ Epoxy laminates studied
were fabricated and all of the material parameters of
laminated composite materials were measured
experimentally. On the contrary, the compressive
strength and failure mechanisms were investigated for
hybrid composites. Static uni-axial compressive tests
were performed on unnotched specimens made from
double-layer of carbon, glass, and Kevlar fibres and
epoxy resin combined to give six different stacking
hybrid composite materials


