May 27, 2014 #1 sobe8 Aerospace May 27, 2014 2 US Can Abaqus calculate the Laminate Equivalent Properties of a shell composite layup? It's really easy to do this in FEMAP, but I haven't figured out how to do this in Abaqus yet. Thanks, Victor
Can Abaqus calculate the Laminate Equivalent Properties of a shell composite layup? It's really easy to do this in FEMAP, but I haven't figured out how to do this in Abaqus yet. Thanks, Victor