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  1. MCR Kumara

    Sap Shell Modeling

    i incresed the mesh then stress is over to calculated one
  2. MCR Kumara

    Sap Shell Modeling

    Maximum Stress = MxY/I = 50x10^6x100/(1/12x100x200^3) = 75(N/mm2)
  3. MCR Kumara

    Sap Shell Modeling

    shell thickness is 100mm and width is 300mm. As cantilever beam i can find stresses using My/E. Load is verical z direction
  4. MCR Kumara

    Sap Shell Modeling

    Shell modeled in X-Z plane and load also applied in along Z axis as cantilever beam. m11 stresses different from calculated stress why?

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