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Scale effects on the response of composite structures under impact loading

机译:冲击载荷作用下尺度对复合结构响应的影响

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摘要

For several years, composite materials have taken a significant part in the realization of structures designed for transport (aeronautical, nautical, automotive. . .). In order to qualify the behavior of such structures, preliminary validation tests have to be done. These specific tests are often very expensive and difficult to set up, especially when the structure dimensions are large (fuselages of aircraft, ship hulls. . .). An alternative way is then to employ small-scale models.The use of these reduced scale structures requires the identification of similitude models allowing the extrapolation of the small-scale model behavior to the real structure. Although largely developed in the case of homogeneous materials, such similitude techniques are not clearly identified for composite materials taking into account the damage evolution duringan impact.The purpose of this article is firstly to present existing similitude techniques making it possible to predict the composite structure behaviour from the knowledge of small-scale model response. Secondly, experiments were done on two scale of samples carried out by stratification of unidirectional carbon/epoxy plies. These results were finally compared with theanalytical predictions of similitude laws currently used.The aim of this paper is to contribute to similitude laws development applied to composite structures. These laws permit to extrapolate the small-scale model behavior to the real scale one. Existing approaches have been established followingtwo different methods. They are summarized in this paper and applied to impact loadings on two laminated plate scales.In order to complete data collected by ‘‘conventional’’ instrumentation (force transducer, displacement sensor, accelerometer.. .), optical device such as an high-velocity CCD camera, associated with optical techniques for the monitoring of markers, were used. These techniques make possible to compare displacement lines corresponding to each scale. It is shown that existing similitude laws, used for elastic materials, do not allow to simulate the behavior of the real scale when this one is damaged.
机译:多年来,复合材料在设计用于运输的结构(航空,航海,汽车...)中发挥了重要作用。为了验证此类结构的行为,必须进行初步的验证测试。这些特定的测试通常非常昂贵且难以设置,尤其是在结构尺寸较大时(飞机机身,船体……)。然后,另一种方法是采用小规模模型。使用这些缩减规模的结构需要识别相似度模型,以允许将小规模模型的行为外推到实际结构。尽管在均质材料的情况下已得到很大发展,但考虑到撞击过程中的损伤演变,这种相似性技术并未明确用于复合材料。本文的目的是首先介绍现有的相似性技术,以预测复合结构的行为。从小规模模型响应的知识。其次,通过对单向碳/环氧树脂层进行分层,对两种规模的样品进行了实验。最后将这些结果与目前使用的相似定律的分析预测进行了比较。本文的目的是为应用于复合结构的相似定律的发展做出贡献。这些定律允许将小规模模型的行为外推到实际规模。现有的方法已经通过两种不同的方法建立。它们在本文中进行了总结,并应用于两个层压板秤上的冲击载荷。为了完成通过“常规”仪器(力传感器,位移传感器,加速度计..),光学设备(例如高强度)收集的数据使用了与用于监视标记的光学技术相关联的高速CCD摄像机。这些技术使得可以比较对应于每个比例尺的位移线。结果表明,现有的用于弹性材料的相似定律不允许模拟真实比例尺的损坏行为。

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