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  • Users: carmenta
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  1. carmenta

    Modeling 2 cell wing box under vertical shear loading [FEMAP] help

    Hello all, I have a two cell wing box cell structure that has been idealized as concentrated areas for the flanges and stiffeners. The spar flanges and stiffeners are assumed to carry only axial loads and the skin and spar webs are assumed to take only the shear loads. My question is how would I...
  2. carmenta

    Modeling 2 cell wing box under vertical shear loading [FEMAP] help

    Hello all, I have a two cell wing box cell structure that has been idealized as concentrated areas for the flanges and stiffeners. The spar flanges and stiffeners are assumed to carry only axial loads and the skin and spar webs are assumed to take only the shear loads. My question is how would...

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