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...
im new at ansys and im modeling a complete wing structure but im having problems when i apply loads, the wing do not deforms along with ribs and spars, only one of them deforms