Abstract
Cracks occurring at arbitrary orientations in lamellar composites are studied. The associated boundary value problem is formulated in terms of dual integral equations in which the kernels are found in series form. This series representation of the kernels is shown to converge quite rapidly. Variation of the stress intensity factors with the constituent elastic moduli is presented, and a comparison of calculated values with a Mohr's circle approximation of the stress intensity factors at arbitrary orientations is made. This comparison results in the conclusion that the Mohr's circle approximation is accurate as long as the crack tip is far enough from the bimaterial interface.
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