《Table 1 Material parameters for T700 fiber/epoxy composite layers (Tan et al., 2015;Wang et al., 20

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《考虑自增强影响的Ⅲ型复合材料气瓶连续损伤模拟及渐进失效分析（英文）》

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In order to validate the progressive failure method based on the Hashin failure criteria and 3D strain-based damage evolution laws in this study，numerical codes are developed using ABAQUS-UMAT to implement the implicit FEA algorithm.It is also compared with the experimental result（Liu et al.，2012c）.T700 fiber/epoxy composite specimens with a 10 mm central hole are used in the test.The lay pattern and geometry size are[0°/45°/90°/-45°]2s and 250 mm×25 mm×1.8 mm，respectively.The thickness of each ply is 0.1125 mm.Material parameters for T700 fiber/epoxy composite layers are listed in Table 1.