Complex stress fields develop during the loading of glass/polymer laminates
used as architectural safety glazing due to: (1) large glass/polymer modul
us mismatch (E-glass/E-polymer similar to 10(3)-10(5)), (2) polymer viscoel
asticity, and (3) nonlinear, large deflection behavior encountered in comme
rcial scale glazing. We present a model for stress analysis of such laminat
es that consists of a three-dimensional finite-element model incorporating
polymer viscoelasticity and large deformations. The model has been applied
to study quasi-static deformation of a square, simply supported, glass/poly
vinyl butyral/glass laminate in response to uniform pressure loading. One o
f the major findings is that stress development may fall outside the so-cal
led "monolithic" limit, for two well-bonded pieces of glass, and the "layer
ed" limit, for two freely sliding plates. One reason is because deformation
of large plates prior to glass first cracking includes considerable membra
ne stresses and the monolithic and layered limits are derived for the case
of small bending deflections of beams. We also find that stress development
is influenced by temperature (or loading rate), particularly in the vicini
ty of the polymer glass transition temperature. However, the effect of temp
erature can be diminished at large deflections as membrane stresses dominat
e and coupling between glass plies plays a lesser role in stress developmen
t. A method is presented to compute the probability of glass first cracking
by combining our finite-element-based stress analysis with a Weibull stati
stical description of glass fracture. One surprising result of the analysis
is that for typical glass Weibull moduli (5-10), the Weibull effective str
ess used to compute the probability of first cracking is only weakly depend
ent on temperature. The stress analysis and failure prediction model presen
ted may be applied to describe the load-bearing capacity of laminates of ar
bitrary shape and size under specified loading and support conditions.