Abstract
Composite laminate plates, fabricated by bonding fiber–reinforced layers, were
dynamically analyzed under different combinations of number of layers, type of cutout, hole
dimensions, angle of lamination and type of dynamic loading . This work was achieved by the
well–known engineering software (ANSYS). The toughness of composite plates was
evaluated in terms of the normal stress in the direction of loading at the periphery of the
cutout. The toughness was found to increase by increasing the number of layers, by setting the
lamination angle at around 40o
,by selecting hole dimensions to width of plate ratio of around
0.4 and by employing square cutouts or avoiding triangular cutouts. Also, composite plates
were found to be more strain-rate-sensitive in ramp loading, with least number of layers and
with triangular type of cutout.
dynamically analyzed under different combinations of number of layers, type of cutout, hole
dimensions, angle of lamination and type of dynamic loading . This work was achieved by the
well–known engineering software (ANSYS). The toughness of composite plates was
evaluated in terms of the normal stress in the direction of loading at the periphery of the
cutout. The toughness was found to increase by increasing the number of layers, by setting the
lamination angle at around 40o
,by selecting hole dimensions to width of plate ratio of around
0.4 and by employing square cutouts or avoiding triangular cutouts. Also, composite plates
were found to be more strain-rate-sensitive in ramp loading, with least number of layers and
with triangular type of cutout.
Keywords
ANSYS
Composite
cutouts
dynamic
finite elements
plates