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Predictions of the frequencies of bending-torsion coupled laminated composite plates with discontinuities: Novel analytical modeling and experimental validation

机译:具有不连续性的弯扭耦合层压复合材料板的频率预测:新型分析模型和实验验证

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摘要

A novel analytical model that accurately represents the free vibration response of intact/damaged composite plates accounting for the bending-torsional coupling is developed. Unlike the existing models for the bending-torsion vibrations of composite plates, in the present model, the equations of motion are derived in an uncoupled form. It is then easier to derive analytical solutions for composite plates under coupled bending-torsion vibrations. In addition, for the first time, analytical solutions for the free bending and torsional vibrations of cantilever and clamped-clamped laminated composite plates with discontinuities including circular holes, rectangular holes, notches, and internal and edge cracks are easily obtained. Shifts in the natural frequencies due to discontinuities are modeled where the reductions in the plate stiffnesses are related to the amount of the energy release rate due to a defect formation. In order to verify the accuracy of the proposed model and the derived solutions, the proposed model is compared to the available conventional models. Moreover, experimental measurements of the free bending and torsional vibrations of carbon-fiber-laminated composite plates with circular holes is performed. A set of finite element analyses are carried out and compared to the experimental and the proposed model results. Then, a parametric study is presented in order to investigate the effects of the discontinuity size and location on the bending and torsional natural frequencies of laminated composite plates with various forms of discontinuities. The performed analyses demonstrate the accuracy of the proposed models to represent the free vibrations of laminated composite plates with discontinuities. (C) 2017 Elsevier Ltd. All rights reserved.
机译:建立了一种新的分析模型,该模型精确地表示了完整的/损坏的复合板的自由振动响应,并考虑了弯扭耦合。与现有的复合板弯曲扭转振动模型不同,在本模型中,运动方程是以非耦合形式导出的。这样,在耦合弯曲-扭转振动下就更容易得出复合板的解析解。此外,首次轻松获得悬臂和夹固层合复合板的自由弯曲和扭转振动的解析解,该复合板的不连续性包括圆形孔,矩形孔,缺口以及内部和边缘裂纹。对由于不连续而引起的固有频率的变化进行了建模,其中板刚度的降低与由于缺陷形成而导致的能量释放速率的大小有关。为了验证提出的模型和派生解决方案的准确性,将提出的模型与可用的常规模型进行比较。而且,进行了具有圆孔的碳纤维层压复合板的自由弯曲和扭转振动的实验测量。进行了一组有限元分析,并与实验和拟议的模型结果进行了比较。然后,进行参数研究,以研究不连续尺寸和位置对具有各种不连续形式的层压复合板弯曲和扭转固有频率的影响。进行的分析证明了所提出模型的正确性,以代表具有不连续性的层压复合板的自由振动。 (C)2017 Elsevier Ltd.保留所有权利。

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