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Nonlinear Shell Modeling of Thin Membranes with Emphasis on Structural Wrinkling

机译:薄膜的非线性壳模型,以结构起皱为重点

摘要

Thin solar sail membranes of very large span are being envisioned for near-term space missions. One major design issue that is inherent to these very flexible structures is the formation of wrinkling patterns. Structural wrinkles may deteriorate a solar sail's performance and, in certain cases, structural integrity. In this paper, a geometrically nonlinear, updated Lagrangian shell formulation is employed using the ABAQUS finite element code to simulate the formation of wrinkled deformations in thin-film membranes. The restrictive assumptions of true membranes, i.e. Tension Field theory (TF), are not invoked. Two effective modeling strategies are introduced to facilitate convergent solutions of wrinkled equilibrium states. Several numerical studies are carried out, and the results are compared with recent experimental data. Good agreement is observed between the numerical simulations and experimental data.
机译:可以设想将大跨度的薄太阳帆膜用于近期的太空飞行。这些非常灵活的结​​构所固有的一个主要设计问题是起皱图案的形成。结构性起皱可能会破坏太阳帆的性能,在某些情况下会破坏结构的完整性。在本文中,使用ABAQUS有限元代码采用几何非线性,更新的拉格朗日壳公式,以模拟薄膜中起皱变形的形成。不会引用真实膜的限制性假设,即张力场理论(TF)。引入了两种有效的建模策略来促进皱纹平衡态的收敛解。进行了一些数值研究,并将结果与​​最新的实验数据进行了比较。在数值模拟和实验数据之间观察到良好的一致性。

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