In other studies dealing with the edge effect in composite materials [1-5] each layer was regarded as an anisotropic homogeneous one, all layers rigidly joined together and the entire specimen in a state of generalized plane strain under tension or flexure. The equations of anisotropic elasticity were solved by the finite-difference method [i, 2], by the finite-element method [3, 4], or by expansion into a double series of Legendre polynomials [5]. In the way these methods have been used, however, they hardly yield a true description of the edge effect with respect to stresses, because they are efficacious only when a bounded function will be the solution and not when the stresses can have singularities, as in the case of composite materials. In the application of these methods, the edge stresses remain bounded, but their maximum increases with increasing accuracy of the method (e.g., with an increasing number of terms retained in the series of orthogonal polynomials [5]) and this indirectly confirms the existence of a singularity. Here it will be demonstrated that in composite materials with characteristics close to real, there may appear a stress singularity, then there will be given examples of calculating the degree of such a singularity as a function of the reinforcement factor and of the fiber lay angle in adjacent layers of the composite
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