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The static and dynamic behaviour of carbon fibre composites used in golf club shafts

机译:用于高尔夫球杆杆身的碳纤维复合材料的静态和动态特性

摘要

The static and dynamic properties of carbon fibre composites of varying orientation, stacking sequence and geometry has been analysed in terms of modulus and material loss factor up to strain rates applicable to golf club shafts. No noticeable change in modulus or damping was seen at strain rate applicable to golf club shafts. All panels tested strain rate sensitivity onset occurred at around 0.4 s(^{-1}), which is above the maximum observed during a golf swing (0.1 s(^{-1})). The strain rate sensitivity was found to be sensitive to aspect ratio (for strain rates above 0.4 s(^{-1})). Two 20° panels of the same fibre interfacial area, but with different aspect ratios (length/width) showed different strain rate sensitivities. The short wide panel (aspect ratio 1.5) showed a higher stiffness and lower strain rate sensitivity when compared to a panel with an aspect ratio of 2.6. A model was created to predict the modulus and damping of lay-ups for laminates and golf club shafts. The model was validated against three composite systems at varying orientations and stacking sequences. The software agreed well with laminate experimental data (data sets showed a RMSD of less than 5 %). From this an optimising software was developed to provide the user with a stacking sequence that will optimise modulus, damping or the product of both. This thesis also evaluated commercial shafts in order to determine the models applicability to this application. Commercial shafts were tested for both stiffness and damping, where a number of aspects such as inter-ply resin rich regions and seam were observed as possible areas for discrepancy with the models prediction. Shafts were fabricated in order to analyse these aspects in greater deal, and to determine the models limits for this application. The model accurately predicted the stiffness of the shafts however the model failed to predict the damping of the shafts when comparing to the average values taken. When damping was compared to the areas where no seams were present, the model agreed well except for in two cases, which have been attributed to shafts flaws (cracks or excess inter ply resin). The model presented in this research consistently characterised the stiffness of fabricated shafts, however the seams proved too dominant a feature to be neglected in the prediction of damping.
机译:根据模数和材料损耗因子,直至适用于高尔夫球杆杆身的应变速率,分析了不同取向,堆叠顺序和几何形状的碳纤维复合材料的静态和动态特性。在适用于高尔夫球杆杆身的应变速率下,模量或阻尼没有明显变化。所有面板测试的应变率敏感度开始发生在大约0.4 s (^ {-1} ),高于高尔夫挥杆期间观察到的最大值(0.1 s (^ {-1} ))。发现应变率敏感性对纵横比敏感(对于高于0.4 s (^ {-1} )的应变率)。具有相同纤维界面面积但纵横比(长度/宽度)不同的两个20°面板显示出不同的应变速率敏感性。与宽高比为2.6的面板相比,短而宽的面板(宽高比为1.5)显示出更高的刚度和更低的应变速率敏感性。创建了一个模型来预测层压板和高尔夫球杆杆身的叠层的模量和阻尼。该模型针对不同方向和堆叠顺序的三个复合系统进行了验证。该软件与层压板实验数据非常吻合(数据集的RMSD小于5%)。由此开发了一个优化软件,为用户提供了可以优化模量,阻尼或两者之积的堆叠顺序。本文还评估了商用轴,以确定该模型对本应用的适用性。对商用轴进行了刚度和阻尼测试,其中观察到许多方面,例如层间树脂富集区域和接缝,可能与模型预测有差异。为了更好地分析这些方面并确定此应用的模型限制,制造了轴。该模型准确地预测了轴的刚度,但是当与所取的平均值进行比较时,该模型无法预测轴的阻尼。将阻尼与没有接缝的区域进行比较时,该模型非常吻合,除了在两种情况下,这归因于轴缺陷(裂纹或中间树脂过多)。这项研究中提出的模型始终如一地描述了装配式轴的刚度,但是接缝被证明是太重要的特征,在预测阻尼方面是可以忽略的。

著录项

  • 作者

    Slater Carl;

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  • 年度 2012
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  • 原文格式 PDF
  • 正文语种 {"code":"en","name":"English","id":9}
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