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Non-linear dynamic thermo-mechanical buckling analysis of the imperfect sandwich plates based on a generalized three-dimensional high-order global-local plate theory

机译:基于广义三维高阶全局局部板理论的非理想夹层板非线性动力热机械屈曲分析

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摘要

The available plate theories either have not considered the interlaminar stress continuity condition or have been calibrated based on linear strain-displacement relations. Moreover, almost all buckling analyses performed so far employing the global-local plate theories, were restricted to linear, static buckling analyses of the perfect plates, neglecting the transverse normal strain and stress. Researches available in literature for dynamic buckling analyses of the sandwich plates are very rare. In the present paper, a generalized high-order global-local theory that satisfies all the kinematic and transverse stress continuity conditions at the interfaces of the layers, is proposed to investigate dynamic buckling of imperfect sandwich plates subjected to thermo-mechanical loads. In comparison to the layerwise, mixed, and available global-local theories, the present theory has the advantages of: (1) less required computational time due to using the global-local technique and matrix formulations, (2) higher accuracy due to satisfying the complete interlaminar kinematic and transverse stress continuity conditions and considering the transverse flexibility, (3) suitability for non-linear analyses, (4) capability of investigating the local phenomena, such as the wrinkling. To enhance the accuracy of the results, compatible Hermitian quadrilateral elements are employed. The buckling loads are determined based on a criterion previously published by the author.
机译:可用的板理论或者没有考虑层间应力连续性条件,或者已经基于线性应变-位移关系进行了校准。而且,到目前为止,几乎所有使用整体局部板理论进行的屈曲分析都局限于对理想板的线性,静态屈曲分析,而忽略了横向法向应变和应力。文献中对夹层板进行动态屈曲分析的研究很少。在本文中,提出了一种满足各层界面上所有运动学和横向应力连续性条件的广义高阶全局局部理论,以研究不完善夹心板在热机械载荷作用下的动态屈曲。与分层,混合和可用的全局局部理论相比,本理论具有以下优点:(1)由于使用了全局局部技术和矩阵公式,因此所需的计算时间更少;(2)由于满足了较高的精度完整的层间运动学和横向应力连续性条件,并考虑横向柔韧性,(3)适用于非线性分析,(4)研究局​​部现象(例如起皱)的能力。为了提高结果的准确性,使用了兼容的Hermitian四边形元素。屈曲载荷是根据作者先前发布的标准确定的。

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