In this paper the friction and wear behavior of a carbon composite is studi
ed. Friction tests were performed under constant friction model The power i
nputs were increased gradually to study their effects on friction transitio
n at ambient air environment. Friction surfaces were examined using various
macro and nanoscopic techniques to understand the evolution of friction tr
ansition. Structural changes of friction film have been observed from graph
itic allotropic form to amorphous type structure. This sudden change leads
to an increase of the coefficient of friction. It seems that the inter-lami
nar shearing, disruption of the film and sample cracking might cause the fr
iction transition. Analysis from stress field simulation shows that cracks
were more likely to occur at the trailing edge of the sample at the end of
transition. This study shows that any type of failure (mechanical or therma
l,fatigue) of the friction film or bulk material is sufficient to generate
friction and wear instabilities.