I was wondering if anybody has experience using the NEi Nastran tension only shell element. It has been a common challenge at the aerospace companies I have worked at to properly idealize the buckled behavior of thin aircraft skins and panels in a finite element model, especially at the vehicle...
Just wanted to tell you all that there is a new web site that has been set up as a resource for ANSYS users. There are quite a few ANSYS white papers, an FAQ and some tutorials all available on the site. You don't need to register or anything....
http://ansys.belcan.com
Paul
When modeling a composite laminate using MSC.Nastran the PCOMP and MAT8 (or MAT1) entries are converted before the run to an equivalent PSHELL and four MAT2 entries which are used in the actual Nastran run. I understand that three of these MAT2 cards are calculated from classical lamination...