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Nonlinear finite element model for the analysis of axisymmetric inflatable beams

机译:轴对称充气梁分析的非线性有限元模型

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Inflatable structures are already being used for decades now especially in aerospace applications. The Inflatoplane and inflatable space habitats are just examples. On the other hand, the modeling and simulation techniques of inflatable structures are lacking far behind. Most of the available models are concerned with cylindrical beams. In this paper, a nonlinear Finite Element model for axisymmetric inflatable structures is developed using beam elements. The model is validated by comparing its predictions to two cases of cylindrical beams in the literature. The model is then utilized to predict the effect of two parameters on the wrinkling load of the beam. Results show that the wrinkling load is proportional to the square root of the inflation pressure. For the beam radius, it is proportional to the cube of the radius at small radii but then the relation is linear afterwards. The model is also used to predict the performance of an inflated truncated cone as a function of the inflation pressure and the root radius. The proposed nonlinear Finite Element model is a step towards analyzing real-life inflatable structures. (c) 2015 Elsevier Ltd. All rights reserved.
机译:充气结构已经使用了数十年,尤其是在航空航天应用中。充气飞机和充气空间栖息地只是示例。另一方面,充气结构的建模和仿真技术远远落后。大多数可用的模型都与圆柱梁有关。在本文中,使用梁单元开发了轴对称可膨胀结构的非线性有限元模型。通过将模型的预测结果与文献中的两种圆柱梁情况进行比较来验证该模型。然后,利用该模型预测两个参数对梁的起皱载荷的影响。结果表明,起皱载荷与膨胀压力的平方根成正比。对于光束半径,它与小半径下的半径的立方成正比,但之后关系为线性。该模型还用于根据充气压力和根部半径来预测膨胀的圆锥台的性能。提出的非线性有限元模型是分析现实生活中的充气结构的一步。 (c)2015 Elsevier Ltd.保留所有权利。

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