Abstract

All parameters of revised Ladevèze failure criterion in Table 1 were determined based on mechanical tests which mainly include quasi-static tensile experiments, quasi-static compressive experiments, quasi-static tensile cyclic loading experiments, the dynamic tensile experiments, dynamic compressive experiments, quasi-static and dynamic inter-laminar shear experiments. The quasi-static experiments were performed using an electronic universal testing machine with a maximum load capacity of 10KN, and the split Hopkinson pressure bar (SHPB) and split Hopkinson tension bar (SHTB) were employed in dynamic experiments. In addition, the parameters of traditional orthogonal anisotropic model and cohesive layer for the laminated plates are listed in Table 2.

Highlights

  • How data was acquired The data are acquired from quasi-static and dynamic mechanical experiments based on electronic universal testing machine CSS-44100, split Hopkinson pressure bar (SHPB) and split Hopkinson tensile bar (SHTB)

  • All these parameters were determined based on mechanical tests by referring to the ASTM standards

  • The quasi-static experiments were performed using an electronic universal testing machine, the strains of specimens were collected by strain gauges as well as the loads were collected by load sensor

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Summary

Data accessibility

Related research article Author's name: Cunxian WANG, Tao SUO, Chao HANG, Yulong LI, Pu XUE, Qiong DENG. Since strain rate effect of composites is considered, simulations with the support of experimental data corresponding to Ladeveze failure criterion can predict the damage mechanisms better than traditional biphasic model under high-velocity impact loading condition, which can significantly reduce research costs. The data presented contains Ladeveze constitutive parameters of unidirectional carbon-epoxy material and orthotropic material properties for composites and cohesive element. The damage kinematics of the elementary layer of Ladeveze failure criterion can be depicted as follows [2]: Global constitutive relation: Àv012 0

ÀvE0112
 10À5 or dn À dnÀ1
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