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首页> 外文期刊>Journal of Applied Mechanics: Transactions of the ASME >The Two-Dimensional Elasticity Solution for the Buckling of a Thick Orthotropic Ring Under External Pressure Loading
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The Two-Dimensional Elasticity Solution for the Buckling of a Thick Orthotropic Ring Under External Pressure Loading

机译:外力作用下厚正交异性环屈曲的二维弹性解

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摘要

This paper is concerned with the 2D elasticity solution for the buckling of a thick orthotropic ring under external hydrostatic pressure loading. The bifurcation buckling problem is first formulated using two methods, distinguished by the manner in which the external work done by the pressure loading during the buckling transition is treated. In doing so, the correct buckling equations and associated traction boundary conditions are derived. The resulting sets of equations and associated boundary conditions are then cast in a weak form, amenable to a numerical solution using the finite element method. The necessity of using the correct pairs of energetically conjugate stress and strain measures for the buckling problem is pointed out. Errors in using the incorrect traction boundary condition and terms that influence the buckling load and that have been omitted in popular commercial codes are pointed out and their significance in influencing the buckling load is identified. Results from the present two-dimensional analysis to predict the critical pressure are compared with previous theoretical results. The formulation and results presented here can be used as the correct benchmark solution to establish the accuracy in computing the buckling load of thick orthotropic composite structures, of contemporary interest, due to the increased use of thick-walled composite shell type structures in diverse engineering applications.
机译:本文涉及在外部静水压力载荷下厚正交异性环屈曲的二维弹性解。分叉屈曲问题首先使用两种方法来表述,其区别在于处理屈曲过渡过程中由压力载荷完成的外部功的方式。这样,可以得出正确的屈曲方程式和相关的牵引力边界条件。然后将所得的方程组和关联的边界条件集转换为弱形式,以使用有限元方法进行数值求解。指出了使用正确的能量共轭应力和应变对对解决屈曲问题的必要性。指出了使用不正确的牵引边界条件和影响屈曲载荷的术语的错误,这些术语在流行的商业法规中已被忽略,并指出了它们在影响屈曲载荷中的重要性。本二维分析预测临界压力的结果与以前的理论结果进行了比较。由于在各种工程应用中越来越多地使用厚壁复合壳型结构,因此,本文介绍的公式和结果可作为正确的基准解决方案,以确立计算厚正交异性复合结构的屈曲载荷的精度,具有当代意义。 。

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