Friday, May 10, 2013

Multiple delamination of a L-shaped composite laminate. There are 15 plies with stacking [0/90/0/90..]. NURBS elements are used to model the plies and the cohesive interfaces.

Monday, May 6, 2013

Delamination of a L-shaped composite (15 plies of 0/90 unidirectional fiber reinforced epoxy/carbon) using Isogeometric Analysis (IGA). Pre-processing is performed using MIGFEM and solved with jem/jive C++ code. Post-processing is done in Matlab and Paraview.