A crack interaction method for cracks in anisotropic fibrous composites is presented. The method is bused on the idea of superposition of resultant tractions along the crack faces. The unknown tractions are expressed by a series of base functions which describe the fundamental solution of stress induced by a solitary crack in an infinite elastic medium, loaded by any such functions. The method employed herein falls within the scope of two-dimensional elasticity but may analogously be applied to other three-dimensional problems (penny-shaped cracks). From the results of various crack configurations in unidirectional fibrous reinforced materials, it is shown that the stress intensity factors strongly depend on the axial to transverse stiffness ratio. Finally, some typical examples, which highlight specific features of the method in different composite material systems are considered and compared to other existing results.
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