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Dynamic initiation and propagation of cracks in unidirectional composite plates.

机译:单向复合板中裂纹的动态萌生和扩展。

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摘要

Dynamic crack growth along weak planes is a significant mode of failure in composites and other layered/sandwiched structures and is also the principal mechanism of shallow crustal earthquakes. In order to shed light on this phenomenon dynamic crack initiation and propagation characteristics of a model fiber-reinforced unidirectional graphite/epoxy composite plate was investigated experimentally. Dynamic fracture experiments were conducted by subjecting the composite plates to in-plane, symmetric and asymmetric, impact loading. The lateral shearing interferometric technique of coherent gradient sensing (CGS) in conjunction with high-speed photography was used to visualize the failure process in real time. It was found that mode-I cracks propagated subsonically with crack speeds increasing to the neighborhood of the Rayleigh wave speed of the composite. Also in mode-I, the dependence of the dynamic initiation fracture toughness on the loading rate was determined and was found to be constant for low loading rates and to increase rapidly above K&d2;dI10 5 . The dynamic crack propagation toughness, KID, was observed to decrease with crack tip speed up to the Rayleigh wave speed of the composite.; For asymmetric, mode-II, types of loading the results revealed highly unstable and intersonic shear-dominated crack growth along the fibers. These cracks propagated with unprecedented speeds reaching 7400 m/s which is the dilatational wave speed of the composite along the fibers. For intersonic crack growth, the interferograms, featured a shock wave structure typical of disturbances traveling with speeds higher than one of the characteristic wave speeds in the solid. In addition high speed thermographic measurements are conducted that show concentrated hot spots behind the crack tip indicating non-uniform crack face frictional contact.; In addition, shear dominated dynamic crack growth is investigated along composite/Homalite interfaces subjected to impact loading. The crack growth phenomenon was observed using dynamic photoelasticity in conjunction with high-speed photography. Three quantized intersonic and supersonic crack tip speed regimes were identified. First conclusive evidence of crack growth at supersonic speeds with respect to lower speed material and sonic speeds with respect to the unidirectional composite was obtained. Furthermore, this investigation documents the first experimental observation of a mother/daughter crack mechanism allowing a subsonic crack to evolve into an intersonic crack.
机译:沿弱平面的动态裂纹扩展是复合材料和其他层状/夹层结构破坏的一种重要方式,也是浅地壳地震的主要机制。为了阐明这种现象,对模型纤维增强的单向石墨/环氧树脂复合板的动态裂纹萌生和扩展特性进行了实验研究。通过使复合板经受面内,对称和不对称的冲击载荷来进行动态断裂实验。相干梯度传感(CGS)的横向剪切干涉技术与高速摄影技术一起用于实时可视化故障过程。研究发现,I型裂纹以亚音速扩展,裂纹速度增加到复合材料的瑞利波速附近。同样在模式I中,确定了动态初始断裂韧度对加载速率的依赖性,发现在低加载速率下它是恒定的,并且在 K 之上迅速增加。 ac> &d2; d I 。动态裂纹扩展韧性 K ID 随着裂纹尖端速度直至复合材料的瑞利波速度而降低。对于II型不对称载荷,结果表明沿纤维高度不稳定且以声速剪切为主的裂纹扩展。这些裂纹以前所未有的速度传播,达到7400 m / s,这是复合材料沿纤维的扩张波速。对于音速裂纹扩展,干涉图具有冲击波结构,该冲击波结构是典型的扰动,其传播速度高于固体中特征波速度之一。另外,进行高速热成像测量,显示裂纹尖端后面的集中热点,表明裂纹面摩擦接触不均匀。另外,还研究了沿冲击载荷作用的复合材料/ Homalite界面的剪切为主的动态裂纹扩展。使用动态光弹性结合高速摄影观察到了裂纹扩展现象。确定了三种量化的音速和超音速裂纹尖端速度方案。获得了关于低速材料在超声速下裂纹扩展和相对于单向复合材料的声速裂纹扩展的第一结论性证据。此外,该研究记录了母子裂纹机理的第一次实验观察,该机理允许亚音速裂纹发展为音速裂纹。

著录项

  • 作者

    Coker, Demirkan.;

  • 作者单位

    California Institute of Technology.;

  • 授予单位 California Institute of Technology.;
  • 学科 Engineering Aerospace.; Engineering Materials Science.
  • 学位 Ph.D.
  • 年度 2001
  • 页码 162 p.
  • 总页数 162
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空、航天技术的研究与探索;工程材料学;
  • 关键词

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