拉挤玻璃纤维复合材料在拉伸-压缩疲劳后的压缩残余强度

IF 5.3 Q2 MATERIALS SCIENCE, COMPOSITES
Aleksandr Elkin, Stepan Konev, Alexander Safonov, Sergey Gusev, Ivan Sergeichev
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引用次数: 0

摘要

我们通过实验测定了拉挤玻璃纤维层压板在拉伸-压缩循环加载后残余抗压强度的下降情况。拉伸-压缩疲劳试验使用的是经过改装的 Arcan 钻机。循环载荷的临界应力比为 R=-0.87。在施加预定次数的应力幅值为 242 兆帕和 173 兆帕的循环加载后,测定了残余抗压强度。结果表明,在应力振幅为 242 兆帕的情况下,疲劳寿命达到 77% 时,残余抗压强度降低了约 20%;在应力振幅为 173 兆帕的情况下,疲劳寿命达到 83% 时,残余抗压强度降低了约 20%。微观结构分析表明,裂纹生长路径和破坏模式取决于应力振幅。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Compressive residual strength of the pultruded glass-fiber composite after tension-compression fatigue

We experimentally determined the decrease of residual compressive strength of the pultruded glass-fiber laminate after tension-compression cyclic loading. The adapted Arcan rig was used for tension-compression fatigue tests. The cyclic load was applied with the critical stress ratio R=−0.87. The residual compressive strength was determined after applying the predefined number of loading cycles with the stress amplitudes of 242 MPa and 173 MPa. The results indicated that the residual compressive strength was reduced about 20% at 77% of fatigue life under the stress amplitude of 242 MPa and at 83% of fatigue life under the stress amplitude of 173 MPa. The microstructural analysis showed that the crack growth path and failure mode depend on the stress amplitude.

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来源期刊
Composites Part C Open Access
Composites Part C Open Access Engineering-Mechanical Engineering
CiteScore
8.60
自引率
2.40%
发文量
96
审稿时长
55 days
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