Nonlinear Behavior of Laminated Composites

  • H.T. Hahn
    Nonmetallic Materials Division Air Force Materials Laboratory Wright Patterson Air Force Base, Ohio 45433

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<jats:p> This paper extends the nonlinear behavior of unidirectional laminae of Reference [1] to that of laminated composites. A comparison between the theory and experimental results is shown through the analysis of uniaxial tension behavior of various laminates. The effect on buckling stress owing to nonlinearity is illustrated for a ±45° angle-ply laminate with simply- supported edges. </jats:p>

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