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  1. Ash_w1

    Wing deflection analysis. Having issue with load distribution

    I did use the create skin option. I managed to add a section to it however I realize now that it just added more stiffness to the wing. Im afraid the modal analysis didn't help either. I've got no clue on how to proceed with this. Surely there is a way to ensure that the pressure force does...
  2. Ash_w1

    Wing deflection analysis. Having issue with load distribution

    I believe it's an error with how i've defined the skin. in the property section, i have defined an area of the model to be a skin. I have applied a shell homogenous section property to it. however, when i go to run the job, ABAQUS says there is no section assigned to the skin area. Do you know...
  3. Ash_w1

    Wing deflection analysis. Having issue with load distribution

    Hello! I am conducting a wing deflection analysis on an aircraft wing. the wing skin and spar were modelled in abaqus as separate parts. they were then assembled together using tie constraints. The ribs for the wing were defined as MPC beam constraints. I applied a pressure load on the bottom...

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