04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
PROCESS MODELLING OF COMPOSITES USING A MULTISCALE FRAMEWORK
G.M. Odegard, Michigan Technological University, United States; M. Maiaru, Columbia University, United States
The goal of this research is to use molecular dynamics (MD) and finite element analysis (FEA) to predict the residual stresses in composite laminates and optimize processing parameters to minimize the residual stress