An efficient analytical method for calculating interlaminar stress dis
tribution near the straight free edges of generally stacked laminates
under different types of loading conditions is presented. The variatio
n of stresses for each ply are established according to boundary-layer
equilibrium equations. All traction boundary conditions at free edges
and traction continuity at ply interfaces are satisfied. Although the
emphasis is placed on assessing the behavioral characteristics of int
erlaminar stresses for unsymmetric laminates, numerical examples for s
ymmetric cases are also presented and compared with available data for
demonstrating the efficiency and accuracy of this method. All results
show high-stress gradients of interlaminar normal and shear stresses
near the free edge.