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首页> 外文期刊>International Journal of Fatigue >Fatigue damage and fatigue limits of a GFRP angle-ply laminate tested under very high cycle fatigue loading
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Fatigue damage and fatigue limits of a GFRP angle-ply laminate tested under very high cycle fatigue loading

机译:在极高的循环疲劳载荷下测试的GFRP角板层压板的疲劳损伤和疲劳极限

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摘要

In contrast to fatigue in the low and high cycle fatigue range, the so-called very high cycle fatigue range (>10~7 cycles) has only been investigated to a minor degree. As very high cycle fatigue testing is challenging in many regards, a special high-frequency four-point bending test rig was developed, set up and validated previously. In this recent study, comprehensive experimental results of an angle-ply laminate tested up to 1.5• 10~8 cycles are presented. In addition to initiation and progression of fatigue damage, stiffness degradation and final failure are investigated at seven load levels. Whereas strain and cycle number show the typical logarithmic dependency in the HCF range, the SN-curve is found to flatten out at lower loads due to slower delamination growth. Neither delamination growth nor final failure are observed at the lowest load level indicating the existence of a delamination threshold load and consequently a fatigue limit. Crack initiation behavior is related to results of a cross-ply laminate by means of a static failure criterion-based master curve approach. Furthermore, the effects of test frequency and specimen heating are investigated.
机译:与低和高循环疲劳范围内的疲劳相反,所谓的非常高的循环疲劳范围(> 10〜7个循环)仅进行了较小程度的研究。由于非常高的周期疲劳测试在许多方面都具有挑战性,因此,之前已经开发,设置和验证了专用的高频四点弯曲测试装置。在最近的这项研究中,介绍了在高达1.5•10〜8个循环中测试的角板层压板的综合实验结果。除了疲劳损伤的发生和发展外,还研究了在七个载荷水平下的刚度下降和最终破坏。尽管应变和循环数显示出HCF范围内的典型对数依赖性,但发现SN曲线由于分层速度较慢而在较低载荷下变平。在最低载荷水平下,都没有观察到分层增长或最终破坏,这表明存在分层阈值载荷,因此没有疲劳极限。裂纹萌生行为与基于静态破坏准则的主曲线方法与交叉层压板的结果有关。此外,研究了测试频率和试样加热的影响。

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