The paper considers the load-transfer mechanisms in carbon-fibre/polypropyl
ene matrix model composites subjected to creep loading and subsequent recov
ery. The fibre strains are measured in situ by micro Raman spectroscopy. Th
e coefficient of friction is calculated on the basis of the measured initia
l residual strains and the initial interfacial pressure on the fibre obtain
ed from the Lame solution. A theoretical approach is utilised to describe t
he creep strain in the matrix material. The analysis shows that the load tr
ansfer between the fibre and the matrix is of a mechanical nature governed
by the radial pressure on the fibre and the coefficient of friction. The ca
lculations indicate that this load transfer mechanism will-for longer loadi
ng times-cause the composite to behave as a pure matrix with holes. (C) 199
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