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  • Users: bhagav_n
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  1. bhagav_n

    BUCKLING ANALYSIS OF AIRCRAFT WING

    Hi, I am trying to perform buckling analysis of aircraft wing in MSC Nastran which is modelled in Patran. The wing consists of ribs, skin and spars. I divided lift load by planform area and applied on the wing upper surface as uniform pressure. The Root section nodes are fixed. While performing...
  2. bhagav_n

    BUCKLING ANALYSIS OF AIRCRAFT WING

    Hi, I am trying to perform buckling analysis of aircraft wing in MSC Nastran which is modelled in Patran. The wing consists of ribs, skin and spars. I divided lift load by planform area and applied on the wing upper surface as uniform pressure. The Root section nodes are fixed. While performing...

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