Flattened carbon
nanotubes (flCNTs) naturally form in many carbon
nanotube-based materials and can exhibit mechanical properties similar
to round carbon nanotubes but with tighter packing and alignment.
To facilitate the design, fabrication, and testing of flCNT-based
composites for aerospace structures, computational modeling can be
used to efficiently and accurately predict their performance as a
function of processing parameters, such as reinforcement/matrix cross-linking.
In this study, molecular dynamics modeling is used to predict the
load transfer characteristics of the interface region between the
flat region of flCNTs (i.e., bi-layer graphene) and amorphous carbon
(AC) with various levels and locations of covalent bond cross-linking
and AC mass density. The results of this study show that increasing
the mass density of AC at the interface improves the load transfer
capability of the interface. However, a much larger improvement is
observed when cross-linking is added both to the flCNT–AC interface
and between the flCNT sheets. With both types of cross-linking, substantial
improvements in interfacial shear strength, transverse tension strength,
and transverse tension toughness are predicted. The results of this
study are important for optimizing the processing of flCNT/AC composites
for demanding engineering applications.