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Bending behavior of laminated composite plates using the refined four-variable theory and the finite element method

机译:用精制的四变量理论和有限元方法弯曲复合板的弯曲行为

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The purpose of this work is to analyze the bending behavior of laminated composite plates using the refined fourvariable theory and the finite element method approach using an ANSYS 12 computational code. The analytical model is based on the multilayer plate theory of shear deformation of the nth-order proposed by Xiang et al 2011 using the theory principle developed by Shimpi and Patel 2006. Unlike other theories, the number of unknown functions in the present theory is only four, while five or more in the case of other theories of shear deformation. The formulation of the present theory is based on the principle of virtual works, it has a strong similarity with the classical theory of plates in many aspects, it does not require shear correction factor and gives a parabolic description of the shear stress across the thickness while filling the condition of zero shear stress on the free edges. The analysis is validated by comparing results with those in the literature.
机译:这项工作的目的是利用由ANSYS 12计算码的精细的四变度理论和有限元方法方法分析层压复合板的弯曲行为。 分析模型基于Xiang等人2011提出的Nth序命令的多层板理论,使用Shimpi和Patel 2006开发的理论原则。与其他理论不同,目前理论中未知功能的数量仅限 四,而在其他剪切变形理论的情况下五个或更多。 本理论的制定是基于虚拟作品的原理,在许多方面,它与板的经典理论具有很强的相似性,它不需要剪切校正因子,并在厚度上给予剪切应力的抛物线描述 填充自由边缘零剪切应力的条件。 通过将结果与文献中的结果进行比较来验证分析。

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