含两个三维嵌埋椭圆裂纹的PMMA单轴压缩开裂及力学响应试验研究

Xiaoping Zhou, Yunding Long, Wei Ye
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引用次数: 0

摘要

本文研究了具有两个三维嵌入共面椭圆缺陷的聚甲基丙烯酸甲酯(PMMA)试样在单轴压缩下的开裂和力学响应。实验结果表明,峰值应力和裂纹萌生应力均随裂纹角度的增大先减小后增大,且随裂纹间距的增大呈线性增大。此外,在这些测试样品中出现了五种裂纹模式,包括共面二次裂纹、翼裂纹、花瓣裂纹、反翼裂纹和垂直巨型裂纹。机翼裂纹的扩展长度大约等于预先存在的裂纹的长轴长度。然而,最大宽度大致等于预先存在的椭圆缺陷长轴长度的一半。最终失效模式包括机翼裂纹和垂直巨型裂纹引起的劈裂失效,以及共面二次裂纹和机翼裂纹引起的混合拉剪失效。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental investigations on the cracking and mechanical responses of PMMA samples with two 3D embedded elliptic flaws under uniaxial compression

In this paper, the cracking and mechanical responses are studied for the Polymethylmethacrylate (PMMA) sample with two three-dimensional embedded coplanar elliptic flaws subjected to uniaxial compression. The experimental results indicate that both the peak stress and crack initiation stress first decrease and then increase with increasing flaw angle, and they increase linearly with increasing flaw spacing. Moreover, five crack modes occur in these tested samples, including the coplanar secondary cracks, wing cracks, petal cracks, anti-wing cracks, and vertical giant cracks. The growth length of wing cracks is approximately equal to the length of the long axis of pre-existing flaw. However, the maximum width is roughly equal to half the length of the long axis of pre-existing elliptic flaw. The final failure modes include the splitting failure induced by wing cracks and vertical giant cracks, and the mixed tensile-shear failure induced by coplanar secondary cracks and wing cracks.

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