Nov 8, 2013 #1 Povera36 Aerospace Joined Sep 21, 2013 Messages 2 Location US Does anyone know a closed form expression to approximate the max ILS at the free edge of a composite layup? I have often seen this developed using a FEM or as a double integral. Thanks in advance!
Does anyone know a closed form expression to approximate the max ILS at the free edge of a composite layup? I have often seen this developed using a FEM or as a double integral. Thanks in advance!