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  • 1
    Publication Date: 2019-08-28
    Description: Numerical and experimental results are presented on the pullout phenomenon in composite materials at a high rate of loading. The finite element method was used, taking into account the existence of a virtual shear deformation layer as the interface between fiber and matrix. Experimental results agree well with those obtained by the finite element method. Numerical results show that the interlaminar shear stress is time dependent, in addition, it is shown to depend on the applied load time history. Under step pulse loading, the interlaminar shear stress fluctuates, finally decaying to its value under static loading.
    Keywords: COMPOSITE MATERIALS
    Type: NASA-TM-76530 , Symp. on FRP,; May 31, 1979; Kyoto; Japan
    Format: application/pdf
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