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  1. cguay

    Stress concentration factor in composite structure

    sorry for the typo Kt = 1 + { 2*[ (Ex/Ey)^0.5-nuxy] + Ex/Gxy}^0.5
  2. cguay

    Stress concentration factor in composite structure

    The Kt for a hole in a composite laminate is Kt = 1 + { 2*[(Ex/Ey)0.5-nuxy] + Ex/Gxy }^0.5

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