Need tutorials for stress analysis of aircraft wing usin MSC Nastran/Patran

need tutorials for stress analysis of aircraft wing using MSC Nastran/Patran, i am in cofusion how to apply loads and boundary conditions.Pl help need urgent

Replies

  • Arockia Ruban M
    Arockia Ruban M
    For Stress analysis of aircraft wing using nastran patran, use pressure load on the bottom of skin and boundary condition as fixed at root chord.

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