zazaisthebest
New member
- May 7, 2008
- 2
i have modeled a wing structure made of shell element for the skin and ribs, and beam 188 for the spars using the text file attached, but instead of shell beam for spars i used beam 188 as an I beam and im having problems when i apply the loads and the deformation is not correct because ansys treats the elements separately, please help me solving this problem