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Hi, I am trying to simulate a wing under the bending load case. I am using Shell elements to model the skin and solid elements to model the frame (Spars, stringers, ribs). I am modelling the simulation in a assembly, thus the skin and the frame are two separate parts. I am defining the contact between the skin and the frame as offset bonded. By doing this the whole structure becomes stiffer (I can see that from the resultant displacements and stresses are much lower than first analytical estimations).
Does someone encountered this problem when the stiffness of the whole structure increases due to the offset bonding contact between shells and solids? Could you please help me by answering what is the reason of this behavior.
Thank you!
Solved! Go to Solution.