Looking for some help here. I have a composite laminate in which each ply is represented by a layer of solid elements. There are 8 plies total, with the stacking sequence being [0/45/-45/90]s. A generic MAT9 card is used. When the property field is assigned, a material CID aligned with the ply orientation is used.
Someone mentioned that there is a command that will print out the stiffness matrix for each property relative to a global or fixed coordinate system. The reason I want this is that I need the ply stiffness matrix relative to a certain coordinate system to be used in another application.
Any help would be appreciated.
jetmaker
Someone mentioned that there is a command that will print out the stiffness matrix for each property relative to a global or fixed coordinate system. The reason I want this is that I need the ply stiffness matrix relative to a certain coordinate system to be used in another application.
Any help would be appreciated.
jetmaker