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INDENTATION AND PENETRATION LAW FOR GFRP LAMINATES UNDER IMPACT CONDITIONS

机译:影响条件下GFRP层压板的压痕和渗透法

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Static and low velocity impact tests were carried out on carbon fibre reinforced plastic plates of various thickness, lay up and architecture [1, 2], which where loaded at the centre by hemispherical steel indentors. The tests were performed up to complete penetration, using different impact conditions. The tests were, then, carried out at growing energy levels in order to characterise the damage initiation and propagation. Because of the big number of the parameters involved in the phenomenon, in order to predict the behaviour of the material, semi empirical models were developed [3, 4, 5] on the base of the data collected. In particular, a law to predict the indentation depth, I, as a function of the absorbed energy indicating that the constants appearing in the model are negligibly influenced by the laminate type and thickness, and constraint conditions adopted was developed. The importance of this study was related, especially in aeronautical field, to the BVID concept and the necessity to know the impact energy and, so, the residual strength of the structure, from a simple visual analysis. In general, the dent depth is strongly dependent on many parameters like the particular laminate, its thickness, the constrain conditions, tup geometry and impact speed. The availability of analytical tools for the prediction of indentation under known impact conditions would simplify the problem. It was shown that, if the ratio of the impact energy to the penetration energy is adopted as the independent parameter, the relationship proposed is negligibly affected by the laminate type and thickness. On the other hand, the necessity to know the penetration energy, U{sub}p, conducted to a calculation of a model [4], accounting only for the reinforcement volume and tup diameter. Thanks to this study, it should be possible to have information about the performance of CFRP laminates in terms of impact energy and residual properties through an indentation measurement, knowing the indentor diameter.
机译:在各种厚度,叠加和建筑[1,2]的碳纤维增强塑料板上进行了静态和低速冲击试验,该塑料塑料板[1,2],其中由半球形钢导入在中心装载。使用不同的影响条件,进行测试以完成渗透。然后,在生长的能量水平下进行测试,以表征损伤引发和繁殖。由于现象中涉及的大量参数,为了预测材料的行为,在收集的数据的基础上开发了半经验模型[3,4,5]。特别地,一种预测压痕深度的法律,作为吸收能量的函数,表明模型中出现的常数被层压型和厚度受到忽视影响,并且开发了采用的约束条件。这项研究的重要性有关,特别是在航空领域,从简单的视觉分析到了BVID概念和必要性地了解碰撞能量,因此,结构的残余强度。通常,凹陷深度强烈依赖于特定层压板的许多参数,其厚度,约束条件,TUP几何和冲击速度。在已知的影响条件下预测压痕的分析工具的可用性将简化问题。结果表明,如果采用冲击能量与渗透能量的比例被采用作为独立参数,所提出的关系受到层压型和厚度的疏忽影响。另一方面,需要了解渗透能量的U {Sub} P,用于计算模型[4],仅占加强体积和TUP直径。由于这项研究,通过缩进测量,应该具有关于CFRP层压板的性能的信息,通过压痕测量,知道压痕直径。

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