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Novel Vibration-based Methods for Detecting Delamination Damage in Composite Plate and Shell Laminates

机译:基于振动的新颖方法来检测复合板和壳层板中的分层损伤

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摘要

The paper describes an on-going research effort aimed at detecting the presence of delamination damage in composite panels based upon their higher-frequency structural response. Two alternative damage indexes are examined that facilitate the identification of the location and extent of delaminations. The damage indexes do not require vibration measurements to be performed on the undamaged structure. Use is made of the bending and twisting curvatures corresponding to the higher-frequency mode shapes that are post-processed via two different smoothing techniques. The modal data are obtained via finite element models based on Mindlin theory and including delaminations. These are introduced using a sub-laminate strategy that permits multiple damages to be modelled through the thickness. Various delamination sizes and locations are examined with a random noise superposed on the data in order to ascertain the degree of sensitivity of the damage index to the noise in the experimental data.
机译:本文描述了一项持续的研究工作,旨在基于复合板的高频结构响应来检测其是否存在分层损坏。检查了两个可替代的损坏指数,它们有助于识别分层的位置和程度。损坏指数不需要在未损坏的结构上执行振动测量。使用与通过两种不同的平滑技术进行后处理的高频模式形状相对应的弯曲和扭曲曲率。通过基于Mindlin理论并包括分层的有限元模型获得模态数据。这些是使用亚层压策略引入的,该策略允许通过厚度对多个损伤进行建模。为了确定实验数据中损伤指数对噪声的敏感程度,对各种分层大小和位置进行了检查,并在数据上叠加了随机噪声。

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