On the free-edge stress singularity of general composite laminates under uniform axial strain

[[abstract]]This work presents a rigorous study on the free-edge stress singularity for general composite laminates (except the angle-ply and cross-ply laminates) under uniform axial strain. Based on the general solutions derived for the plies with 0-degree, 90-degrees and arbitrary fiber orientations, the corresponding transcendental characteristic equations of general [theta1/theta2], [theta/0-degree] and [theta/90-degrees] laminates are established by using appropriate near-field boundary conditions, respectively. To avoid numerical errors, the transcendental characteristic equations are expanded by a symbolic operation technique analytically and solved graphically. Hence, once the ply material properties and stacking sequence are known, the accurate characteristics of the free-edge stress singularity of examined composite laminates can be obtained. These will be helpful for the failure analysis of composite materials and structures.[[fileno]]2020224010033[[department]]動機