The debonding mechanism of an interphase in layered and fiber-reinforc
ed composites was investigated with an emphasis on crack deflection an
d penetration. A single-edged notched model consisting of three phases
was analyzed by the boundary element method. The dependence of elasti
c fields involved in the model on elastic constant combinations was re
vealed. Interfacial debonding other than the competition between crack
deflection and penetration may be initiated due to the high tensile a
nd shear stress concentration before a main crack propagates to meet t
he next interface. The ratio of energy release rates for infinitesimal
deflecting and penetrated cracks, defined as R = G(d)/G(p). was compu
ted when a main crack reached an interphase interface. The results obt
ained modified those for two-phase models. Discussion regarding fractu
re sequences observed in Ti-15-3 alloy reinforced with unidirectionall
y aligned SCS-6 fiber was made. (C) 1998 Acta Metallurgica Inc. Publis
hed by Elsevier Science Ltd. All rights reserved.