Based on the classical laminated plate theory, a finite composite plate wit
h multiple elliptical holes is treated as an anisotropic multiple connected
plate. Using the complex potential method in the plane theory of elasticit
y of an anisotropic body, a series solution to the title problem is obtaine
d by means of the Faber series expansion, the conformal mapping and the lea
st squares boundary collocation techniques. Laminate strength is predicted
by using the concept of characteristic curve and the Yamada-Sun failure cri
terion. The effects of the layups, the hole sizes, the ellipticity of the h
oles, the loading conditions, the relative distance between holes, the tota
l number of holes and their locations on the strength of laminates are stud
ied in detail. Some useful conclusions are drawn. (C) 2000 Elsevier Science
Ltd. All rights reserved.