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Analytical buckling analysis of an inflatable beam made of orthotropic technical textiles

机译:正交各向异性技术纺织品制成的充气梁的屈曲分析

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摘要

An analytical approach was considered to study the buckling and the behavior of an inflatable orthotropic beam subjected to uniform compression loads under different boundary conditions. In order to assess the stability of inflatable structures, it is necessary to evaluate the critical load of the inflatable components in their pressurized configurations. First, a 3D inflatable orthotropic beam model based on the Timoshenko's kinematics was briefly introduced: the nonlinearities (finite rotation, follower forces) were included in this model. The nonlinear equilibrium equations were derived from the total Lagrangian form of the virtual work principle: the linearized equations were then obtained. By solving these linearized equations, an analytical expression of the critical buckling load was obtained. This critical buckling load was investigated through several load cases with several boundary conditions. The discrepancy due to the orthotropic character between the present model and the isotropic models found in the literature was evaluated, as well as the influence of the inflation pressure and the fabric mechanical properties on the value of critical load. The buckling mode shapes were also determined. To check the limit of validity of the results, the wrinkling load was also presented in every case.
机译:考虑采用一种分析方法来研究在不同边界条件下承受均一压缩载荷的正交异性充气梁的屈曲和性能。为了评估可充气结构的稳定性,必须评估可充气部件在其加压配置下的临界载荷。首先,简要介绍了基于Timoshenko运动学的3D充气正交各向异性梁模型:该模型包括非线性(有限旋转,跟随力)。从虚拟工作原理的总拉格朗日形式导出非线性平衡方程:然后获得线性方程。通过求解这些线性方程,获得了临界屈曲载荷的解析表达式。通过几种具有几种边界条件的载荷工况研究了临界屈曲载荷。评估了由于本模型与文献中发现的各向同性模型之间的正交各向异性而引起的差异,以及充气压力和织物力学性能对临界载荷值的影响。还确定了屈曲模式形状。为了检查结果的有效性,还提出了每种情况下的起皱负荷。

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