The thermomechanical behavior of continuous-fiber reinforced titanium
based metal-matrix composites (MMC) is studied using the finite elemen
t method. Fiber and interface failures are modeled as discrete damage.
The evolution of matrix failure is considered as continuum damage. A
thermoviscoplastic unified state variable constitutive theory is emplo
yed to capture inelastic and strain-rate sensitive behavior in the Tim
etal(R)-21 s matrix. The SCS-6 fibers are modeled as thermoplastic and
can fail at some prescribed plastic strain to failure. The effects of
residual stresses generated during the consolidation process on the t
ensile response of the composites are considered. Unidirectional and c
ross-ply geometries are studied. Differences between the tensile respo
nses in composites with perfectly bonded, weakly bonded and completely
debonded fiber/matrix interfaces are discussed.