numbercraze
Aerospace
- Jan 7, 2007
- 7
Hello All,
I have analyzed sandwich panels before using PCOMP. Now I am thinking of modeling the core using 3D elements and the face sheet using shell elements. I understand that I would have to use multi point constraints for the transition in elements between the facesheet and the core. Is this a simple task in Patran and how do i do it? Thanks in advance!!
I have analyzed sandwich panels before using PCOMP. Now I am thinking of modeling the core using 3D elements and the face sheet using shell elements. I understand that I would have to use multi point constraints for the transition in elements between the facesheet and the core. Is this a simple task in Patran and how do i do it? Thanks in advance!!