Nrs. Vure et Rd. Kriz, EFFECT OF COOLING RATE AND STACKING-SEQUENCE ON THE FATIGUE BEHAVIOR OF NOTCHED QUASI-ISOTROPIC AS4 PEEK LAMINATES/, Journal of composites technology & research, 18(2), 1996, pp. 127-134
The effect of cooling rate and stacking sequence on fatigue behavior w
as analyzed for notched quasi-isotropic AS4/PEEK laminates. The fatigu
e behavior of fast (475 degrees F/min) and slow (1 degrees F/min) cool
ed specimens of the following two lay-ups was studied: Layup A of (-45
/0/45/90)(s) and Layup B of (45/90/-45/0)(s). All specimens were subje
cted to a load-controlled, tension-tension fatigue loading with a stre
ss ratio R = 0.1 at a frequency of 5 Hz. Damage was monitored by the r
eduction in dynamic stiffness and penetrant enhanced X-radiography. Po
st-failure analysis was carried out by scanning electron microscopy (S
EM). Influence of cooling rate on the fatigue properties was different
in the two stacking sequences investigated. The fatigue behavior chan
ged drastically with the variation in the stacking sequence. A model,
based on a constant strain-to-failure, was developed for life predicti
on and the predicted lives are in good agreement with the experimental
values. To help understand the fatigue behavior of the two stacking s
equences studied, the interlaminar stress distributions were calculate
d with a quasi-3D finite element analysis (FEA) for the regions around
the hole. Specimens of Lay-up A were predicted to be more prone to de
lamination as compared to those of Lay-up B and this is consistent wit
h experimental observations.