The effect of thermal cycling on the properties of a carbon fibre reinforced magnesium composite

Abstract

Effects of thermal cycling on mechanical properties of two unidirectional ultra-high modulus carbon fibre reinforced magnesium composites (P100S/AZ91D) have been investigated. Composite specimens reinforced with ∼50% or 60% fibre volume fraction were thermally cycled between the temperatures of 100 °C and −100 °C, in a vacuum, for up to 100 cycles. Mechanical testing showed there was no change in the bending strength of samples or the associated failure mode during cycling. Composites did, however, exhibit a moderate reduction in bending modulus and interlaminar shear strength during the first few thermal cycles. Little further degradation was observed thereafter. Modifications to the matrix microstructure were examined and related to a change in matrix properties measured via microhardness testing. Composite property degradation was attributed to the formation of microvoids and interfacial sliding in the early stages of cycling. The implications these processes may have on composite application are discussed and it is concluded that based on the limited dependence of mechanical properties to thermal cycling carbon fibre reinforced magnesium shows potential for space applications operating under transient thermal conditions.