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wing parts contact in ansys

wing parts contact in ansys

wing parts contact in ansys

(OP)
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

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