In this study, the cruciform geometry was utilized to evaluate the interfac
ial normal strength in unidirectional glass/epoxy composites using single f
iber specimens. These model specimens were incrementally loaded in tension
to failure using a specially built loading device mounted on the straining
stage of a microscope. The initiation and location of interfacial debonding
was observed in situ by microscopic examination and inspection of photoela
stic fringe patterns and stress-strain data. Analytical modeling using 3-D
FEM revealed that the stress concentration factor (value of radial stress a
t the interface normalized by the externally applied stress) was at maximum
and remained fairly constant (within 10 percent) over two-thirds of the ce
ntral loading region. As a result, interface debonding always occurred in t
he interior of the sample (region initially free of stress singularities),
thus avoiding the influence of free-edge effects on measured debond strengt
hs.