In order to establish design criteria for a turbine disk made of Carbo
n-Carbon (C/C) composites, spin burst tests were performed on quasi-is
otropically laminated C/C composite disks. Un-notched and notched flat
disks were prepared to evaluate the effect of stress concentration on
fracture behavior. Strain measurements during rotation tests revealed
that deformation of the C/C composite disks with or without notches w
as in agreement with analytical or finite element calculations in the
elastic region, which suggests that the test fixtures of the spin test
er have a negligible effect on the deformation of C/C composite disks.
In the spin burst tests, the un-notched C/C composite disks burst at
an average rotation speed of 25000 r.p.m. with a peripheral velocity o
f 393 mis. A comparison between the mean hoop stress averaged over the
radius and the tensile strength of smooth specimen suggests that the
burst of the un-notched C/C composite disks obey the mean stress crite
rion. On the other hand, the fracture toughness criterion was shown to
be applied for the notched specimen. The difference in the fracture c
riterion between the un-notched and the notched C/C composite disks is
believed to correspond to that between the double edge notched specim
ens and specimens with a hole in the static tensile tests, (which was
explained by the difference in the magnitude of the damaged zone where
the stress concentrations would be relaxed).