A thermomicromechanical model of failure is presented based on thermodynami
c principles, that is, using the balancing laws: the conservation of moment
um and the first and second laws of thermodynamics. The model is oriented t
oward damage initiation and damage progression in a composite structure und
er an intense pressure shock wave, A micromechanical damage approach is con
sidered where three damage modes are modeled tensile damage, shear damage,
and interphase or material mismatch discontinuity between the composite's m
atrix and fiber. A homogenization technique is incorporated in the developm
ent to simplify the representation of the nonhomogeneous material. A summar
y of the equations for the thermomicromechanical model of failure is presen
ted where a damage parameter D is defined to characterize the lamina's dama
ge based on energy dissipation. Numerical analyses are presented to demonst
rate the model characterization to damage.