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An experimental study of rate effects on Mode I delamination of z-pinned composite laminates.

机译:速率对Z钉复合材料层压板I型分层的影响的实验研究。

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摘要

Z-pinned laminates are designed to suppress interlaminar fracture. Much interlaminar fracture damage is due to impact, so an experiment was devised to examine loading rate effects on z-pinned composite laminates. Loading rate effects on the Mode I fracture of IM7/8552 carbon/epoxy composite laminates with and without pultruded carbon/epoxy z-pins were investigated using a Flying Wedge test method. Unpinned laminates were found to fracture in continuous stable crack propagation, with a positive correlation between critical Mode I strain energy release rate, GIc, and wedge velocity.;Two different fracture regimes were found in the z-pinned laminates. From quasi-static to 40 m/s wedge velocities fracture occurred in a series of unstable crack propagations followed by complete arrest of the crack. At high velocity, 250 m/s, steady-state crack propagation was observed, where there was continuous crack propagation and the crack tip and wedge traveled at identical velocities. The possibility of a third transitional fracture regime was noted, as it appears that the 50 m/s wedge velocity resulted in a continuously propagating crack whose velocity oscillated about the wedge's constant velocity.;These z-pinned laminates show that both p0, the critical peak crack closure traction exerted by the z-pins, and GIc decrease with increasing wedge velocity in the stop-and-go fracture regime which holds from quasi-static through a wedge velocity of 40 m/s. At a wedge velocity of 40 m/s, there is a maximum reduction from the quasi-static values of over 30% in p0 and over 35% in GIc. The rate effects on p 0 were also found to dominate those directly on the base laminate GIc when determining the total strain energy release rate of the z-pinned laminate.;The ratio of GIc for the 2% z-pin specimens toGIc for the 0.5% z-pin specimens was found to remain relatively constant over the range of wedge velocities studied; no discernible relationship was found between wedge velocity and that ratio. These results suggest that the current widely held modeling assumption of rate independent z-pin tractions is unjustified, and therefore models should be refined to incorporate rate effects. Additionally, designers should consider using additional safety factors when designing z-pinned composite parts that are planned to endure impact loading until rate effects on fracture properties are better understood.
机译:Z钉层压板旨在抑制层间断裂。层间断裂损坏是由于冲击造成的,因此设计了一个实验来研究加载速率对Z钉复合材料层压板的影响。使用飞行楔形试验方法研究了加载速率对IM7 / 8552碳/环氧复合材料层压板有无拉挤型碳/环氧Z销的I型断裂的影响。未钉扎的层压板在连续稳定的裂纹扩展中破裂,在临界模式I应变能释放速率,GIc和楔形速度之间呈正相关。在Z钉扎的层压板中发现了两种不同的断裂方式。从准静态到40 m / s的楔形速度,断裂发生在一系列不稳定的裂纹扩展中,然后完全阻止了裂纹。在250 m / s的高速下,观察到稳态裂纹扩展,其中裂纹持续不断地传播,并且裂纹尖端和楔形体以相同的速度运动。注意到了第三种过渡断裂方式的可能性,因为看来50 m / s的楔形速度会导致裂纹不断扩展,其速度围绕楔形恒定速度振荡;这些Z钉叠层表明p0都是临界值z销施加的最大闭合裂纹牵引力和GIc在止动断裂状态下随着楔形速度的增加而减小,该状态从准静态一直保持到40 m / s的楔形速度。在楔形速度为40 m / s时,准静态值的最大减小量在p0中超过30%,在GIc中超过35%。在确定z固定叠层的总应变能释放率时,还发现了对p 0的速率影响直接作用于基础叠层GIc上的速率影响;; 2%z引脚试样的GIc与0.5的GIc之比发现在所研究的楔形速度范围内,%z销样品保持相对恒定;在楔形速度和该比率之间没有发现可辨别的关系。这些结果表明,目前广泛使用的与速率无关的z销牵引力的建模假设是不合理的,因此应完善模型以包含速率效应。此外,设计人员在设计Z钉复合材料零件时应考虑使用其他安全系数,这些零件计划承受冲击载荷,直到更好地理解断裂性能的速率影响。

著录项

  • 作者

    Schlueter, Andrew M.;

  • 作者单位

    Purdue University.;

  • 授予单位 Purdue University.;
  • 学科 Engineering Aerospace.
  • 学位 Ph.D.
  • 年度 2012
  • 页码 165 p.
  • 总页数 165
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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