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Initial wrinkling and its evolution of membrane inflated cone in bending

机译:膜充气锥弯曲时的初始起皱及其演变

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摘要

The concept of the wrinkling factor is firstly presented to obtain the wrinkling condition. An extremum method is then proposed to predict the critical wrinkling load and the initial wrinkling location by searching the maximum of the wrinkling factor. Here the critical wrinkling load is defined as the ratio of the wrinkling moment versus the initial wrinkling location, which is different from previous definition. The nondimensional analyses show that the critical wrinkling load and the initial wrinkling location are both closely related to the taper ratio of the inflated cone. The critical taper ratio is 1.5 which corresponds to the highest load-carrying efficiency of the inflated cone in bending. The wrinkled region is finally predicted to deeply understand the wrinkling evolution in the bended membrane inflated cone. A series of wrinkling experiments on the inflated cone in bending are performed to verify the accuracy and the validation of the proposed method. The good agreements between the tests and the predictions give confidence to use the extremum method for wrinkling analysis of the inflated load-carrying structures.
机译:首先提出了起皱因子的概念,以获得起皱条件。然后提出了一种极值方法,通过搜索最大的起皱因子来预测临界起皱载荷和初始起皱位置。此处,临界起皱载荷定义为起皱力矩与初始起皱位置的比率,与先前的定义不同。无量纲分析表明,临界起皱载荷和初始起皱位置均与充气锥的锥度比密切相关。临界锥度比为1.5,它对应于充气圆锥体在弯曲时的最高负载效率。最终预测皱纹区域将深刻理解弯曲膜充气锥中的皱纹演变。对充气圆锥体进行了一系列起皱实验,验证了所提方法的准确性和有效性。试验与预测之间的良好一致性使我们有信心使用极值方法对膨胀的承载结构进行皱纹分析。

著录项

  • 来源
    《Thin-Walled Structures 》 |2012年第2012期| p.97-102| 共6页
  • 作者

    C.G. Wang; Z.Y. Du; H.F. Tan;

  • 作者单位

    Center for Composite Materials, Harbin Institute of Technology, Harbin 150080, China, National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China;

    Center for Composite Materials, Harbin Institute of Technology, Harbin 150080, China, National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China;

    Center for Composite Materials, Harbin Institute of Technology, Harbin 150080, China, National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150080, China;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    membrane; inflated cone; wrinkling; extremum method; load-carrying efficiency;

    机译:膜;充气锥皱纹极值法承载效率;

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