The paper is concerned with the determination of edge effect zone in a laminated composite with laminas subject to longitudinal compression. The dependence of the maximum decay length on the ratio between the period of external loading and the structure parameter is studied. The load period depends on the number of unloaded laminas. The decay of the edge effect is analyzed by numerically solving a boundary-value problem of elasticity for piecewise-homogeneous materials and using a quantitative decay criterion for the near-edge normal stresses Keywords: Saint-Venant's edge effect, laminated composite, representative element, piecewise-homogeneous material, end effect decay criterion
Introduction.In studying the edge effect in composite materials, it is of interest to examine the joint influence of external load and material structure on how it decays [1-3, 6, 12]. The dependence of the decay length in coated materials on the ratio between the period of piecewise-constant surface load and the thickness of the coating (which is generally multilayer) as a structure parameter was examined in [1, 3, 6]. It was established there that the ratio of the decay length to the load period monotonically increases with the load period, tending to some constant value. The decay of the edge effect in a laminate with laminas longitudinally compressed by a uniform surface load of constant intensity was studied in [4]. It was shown there that the maximum length of the edge effect, evaluated to within 1%, is equal to one or two structure parameters, the structure parameter being the total thickness of one lamina and one matrix layer. The decay of the edge effect was analyzed in [2] comparing two cases: uniform compression of laminas and the presence of an unloaded lamina. It was shown there that in the presence of an unloaded lamina, the near-edge stresses redistribute resulting in a smaller decay length of the edge effect in the matrix and a greater decay length in the reinforcement, compared with the case of uniformly compressed laminas.The present paper sets out to determine the decay length of the edge effect in a longitudinally compressed laminate and to study the dependence of the decay length on the ratio between the load period and the structure parameter. The load period depends on the number of unloaded laminas. The design model includes a mixed boundary-value problem of elasticity for piecewise-homogeneous materials and a quantitative decay criterion for near-edge normal stresses. The boundary-value problem is solved using the finite-difference method and the concept of base scheme [5,[9][10][11]. To analyze the decay of the edge effect, we will use a stress decay function~( ) ρ x that describes the relative change of the near-edge normal stresses compared with the self-balanced load on the boundary of the domain of interest. The decay length of the edge effect is defined as the distance from the line of application of the self-balanced load to the points where the normal stresses are equal to ρ % of their magnitude on the ...