Wrinkling of thin membranes due to different in-plane loading and boundary conditions has drawn attention of researchers in structural engineering since the development of thin webs for early aircraft structures. More recently, prestressed lightweight membrane structures have been proposed for future space missions, for example solar sails, the next generation space telescope sunshield and space-based radar systems. These structures are often partially wrinkled during operation. The formation of wrinkles alters the load paths and the structural stiffness of the membranes. More importantly its occurrence degrades the surface accuracy of these structures, which is a key design parameter.ududThis dissertation focuses on wrinkling of thin rectangular membranes subjected to uniaxial tension and investigates the onset and profiles of wrinkles using both experimental and numerical approaches.ududAn optical method, which integrates fringe projection method with four-frame phase-shifting technique, pre-conditioned conjugate gradient phase unwrapping algorithm and series-expansion carrier removal technique was developed in order to measure the full-field out-of-plane displacement of membranes, and an optical system was constructed including a uniaxial tension testbed, a LCD projector and a CCD camera. A series of uniaxial tensile tests were carried out on silicone rubber membranes of varying dimensions and aspect ratios in order to investigate the effect of geometric factors such as membrane dimension and aspect ratio on wrinkling onset; and a series of measurements were performed on each membrane at several desired strain levels to understand the evolution of the wrinkles, in particular wrinkle amplitude and wavelength.ududA numerical study was carried out using the commercial finite element software ABAQUS to further understand the important characteristics of wrinkling of thin membranes observed in the physical model. Geometrically nonlinear finite element models of membrane structures were constructed with thin-shell elements. A series of simulations were carried out for different membrane dimensions. The critical buckling load and buckling modes was predicted for each dimension using a pre-buckling eigenvalue analysis. The desirable buckling mode was selected and introduced into the structure as a geometric imperfection. The formation and growth of wrinkles were simulated in the post-buckling analysis. ududFinally, an idea of suppressing wrinkle instabilities of dielectric elastomer membranes using through-thickness electric field was proposed and verified in both experiment and numerical simulations.
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机译:自从为早期飞机结构开发薄网以来,由于不同的平面载荷和边界条件而引起的薄膜起皱引起了结构工程研究人员的关注。最近,已经提出了用于未来太空任务的预应力轻质膜结构,例如太阳帆,下一代太空望远镜遮阳板和天基雷达系统。这些结构在操作过程中经常会局部起皱。皱纹的形成改变了载荷路径和膜的结构刚度。更重要的是,它的出现降低了这些结构的表面精度,这是一个关键的设计参数。 ud ud本论文着重研究单轴拉伸下矩形薄膜的起皱,并通过实验和数值方法研究起皱的发生和轮廓。 ud ud开发了一种光学方法,该方法将条纹投影方法与四帧相移技术,预处理共轭梯度相位展开算法和串联扩展载波去除技术相结合,以测量全场失调。膜的平面位移,并构建了一个光学系统,包括一个单轴拉伸试验台,一个LCD投影仪和一个CCD相机。为了研究诸如膜尺寸和长宽比等几何因素对起皱的影响,对不同尺寸和长宽比的硅橡胶膜进行了一系列的单轴拉伸试验。并在几个所需的应变水平下对每个膜进行一系列测量,以了解皱纹的演变,特别是皱纹幅度和波长的变化。 ud ud使用商用有限元软件ABAQUS进行了数值研究,以进一步了解皱纹的形成。物理模型中观察到的薄膜起皱的重要特征。用薄壳单元构建了膜结构的几何非线性有限元模型。针对不同的膜尺寸进行了一系列模拟。使用预屈曲特征值分析预测了每个尺寸的临界屈曲载荷和屈曲模式。选择所需的屈曲模式,并将其作为几何缺陷引入结构。在屈曲后分析中模拟了皱纹的形成和生长。最后,提出了一种通过厚度方向电场抑制介电弹性体膜皱纹不稳定性的想法,并在实验和数值模拟中得到了验证。
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