Finite element modelling has been used to explore the basic single-fib
re push-out test and a variant in which in-plane tension is simultaneo
usly applied. Comparison with experimental photoelastic data has shown
that shear-lag based analytical models of the test are unreliable, ev
en for the simplest cases. It has been shown that the loading geometry
and, particularly, the presence of thermal residual stresses can affe
ct the interfacial stress state, which often tends to vary significant
ly along the length of the fibre. For a metal-matrix composite, the pe
ak shear stress is predicted to occur near the bottom of the fibre, wh
ich is where debonding is expected to initiate. The proportion of norm
al and shear stresses at the interface can be altered by the applicati
on of in-plane tension. Some previously published experimental tension
ed push-out data for the SiC/Ti system have been interpreted in the li
ght of finite element modelling, allowing an estimate to be made of th
e interfacial coefficient of friction.