Epoxy resins are
used extensively in composite materials for a
wide range of engineering applications, including structural components
of aircraft and spacecraft. The processing of fiber-reinforced epoxy
composite structures requires carefully selected heating and cooling
cycles to fully cure the resin and form strong cross-linked networks.
To fully optimize the processing parameters for effective epoxy monomer
cross-linking and final product integrity, the evolution of mechanical
properties of epoxies during processing must be comprehensively understood.
Because the full experimental characterization of these properties
as a function of degree of cure is difficult and time-consuming, efficient
computational predictive tools are needed. The objective of this research
is to develop an experimentally validated Molecular Dynamics (MD)
modeling method, which incorporates a reactive force field, to accurately
predict the thermo-mechanical properties of an epoxy resin as a function
of the degree of cure. Experimental rheometric and mechanical testing
are used to validate an MD model, which is subsequently used to predict
mass density, shrinkage, elastic properties, and yield strength as
a function of the degree of cure. The results indicate that each of
the physical and mechanical properties evolve uniquely during the
cross-linking process. These results are important for future processing
modeling efforts.