The ply constitutive relations of an energy-based model for distributed mic
rocracking in continuous fiber reinforced metal matrix composites are prese
nted. Simple models for damage progression ave used in conjunction with the
se damage dependent constitutive relations to allow the prediction of fatig
ue life under constant amplitude, isothermal conditions. The microcracking
model is discussed in the context of fatigue analysis of unnotched titanium
matrix composite laminates. Analytical results generated by using this mod
el in a unidirectional laminate analysis algorithm ave presented and compar
ed with experimental results. [S0094-4289(00)03104-2].