“…Physics-based computational models play a key role in predicting damage initiation and propagation as a result of mechanical and thermal loading conditions, simulating the interaction of elastic and electromagnetic waves with the predicted damage, and assessing the current condition of the structure. Because of the complexities associated with aerospace materials, in particular fiber-reinforced composites, damage prediction and quantification studies are often limited to two-dimensional (2D) geometries, linearly elastic constitutive models, prescribed damage initiation location and progression path, and ordered microstructures (Murthy and Chamis, 1986;Freund, 1990;Sankar and Marrey, 1997;Lee and Staszewski, 2003;Swaminathan, Ghosh, and Pagano, 2006;Skoček, Zeman, and Šejnoha, 2008). These assumptions can lead to oversimplification of the problem, and therefore, often result in poor prediction of the critical behavior of these materials.…”