The paper presents a methodology for evaluating the effective stiffness of
unidirectional composite materials with shape memory alloy (SMA) fibers in
the presence of matrix cracks. The solution is obtained for the case where
SMA fibers in the intact composite are in the austenitic phase. However, el
evated stresses in the sections of SMA fibers adjacent to the crack planes
cause the martensitic transformation affecting the stiffness of the materia
l. The solution has to account for thermal residual stresses in SMA and "or
dinary" fibers and in the matrix. The order of magnitude of these stresses
is calculated in the paper for two representative composite systems. As fol
lows from the numerical examples, thermal residual stresses in the SMA fibe
rs increase proportionally to their volume fraction but remain relatively s
mall. However, thermal stresses in the matrix may reach rather high values
reducing the strength of the matrix by a significant factor.