This paper outlines a current effort at improving the compressive stre
ngth of carbon fiber reinforced composites (CFRC) by using a hybrid ca
rbon/glass commingling concept. Prior investigations into the hydrosta
tic strength of thick-section carbon fiber reinforced composite cylind
ers resulted in failures which were significantly lower (50 to 70% of
design pressure) than anticipated. The formation and propagation of fi
ber kink bands at the microscopic level, triggered by the fiber misali
gnment defects formed during the manufacturing process, leading to a s
hear crippling failure at the macroscopic level is the dominant compre
ssive failure mode in the presence of fiber misalignment or waviness.
It is theorized that one way to improve compressive strength is throug
h the use of a commingled (at the tow level) hybrid fiber system. A no
vel fracture mechanics based concept for commingling a small percentag
e of glass with carbon fibers to suppress compressive failures due to
inelastic micro-buckling of fibers and kink band propagation is develo
ped. A Griffith type fracture criterion for a mode II crack growth, ba
sed on the principle of energy balance, is introduced to derive the hi
therto unknown concept of kink toughness (i.e., resistance to kink ban
d propagation), and to determine the required glass-carbon ratio for p
ossible enhancement of toughness against the kink band propagation. Th
e width of a kink, band normalized with respect to a characteristic le
ngth scale, such as thickness of a matrix impregnated fiber tow can be
used as a practical measure for kink toughness. Preliminary experimen
tal data suggest enhancement of the compressive and flexural strengths
of the composite material even with a small percentage (15%) of glass
fibers in commingled hybrid composites. Most significantly, inspectio
n of the failed compression test coupons clearly demonstrates that int
roduction of this small percentage of glass fibers is effective in cha
nging the failure mode away from the catastrophic kink band failure mo
de. Furthermore, it may be noted that the flexural hybrid commingled g
lass/carbon/epoxy composite specimens have failed in tension, which is
in sharp contrast to what has been observed in their baseline carbon/
epoxy counterparts.