• CN:11-2187/TH
  • ISSN:0577-6686

›› 2004, Vol. 40 ›› Issue (12): 90-95.

• 论文 • 上一篇    下一篇

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蜂窝夹芯胞元壳的屈曲特性研究

梁森;陈花玲;梁天锡   

  1. 西安交通大学机械工程学院;中国工程物理研究院第4研究所
  • 发布日期:2004-12-15

BUCKLING STUDY ON A THIN-WALLED CELLULAR SHELL OF HONEYCOMB SANDWICH STRUCTURE

Liang Sen;Chen Hualing;Liang Tianxi   

  1. School of Mechanicaal Engineering,Xi’an Jiaotong University No.4 Institute, China Academy of Engineering Physics
  • Published:2004-12-15

摘要: 以正六边形蜂窝夹芯的胞元壳为例,将Euler细长杆的稳定理论与板壳力学中的稳定理论相结合,提出了薄壁胞元壳轴向受压临界载荷的计算公式和屈曲模态的三重级数表达式。根据胞元壳不同的失效形式,将其分成了短胞元壳、长胞元壳和特长胞元壳,确定了不同类型胞元壳的临界载荷控制方程和其对应的一阶屈曲模态,在此基础上提出了胞元壳临界载荷总图。用3D有限元数值模拟技术,通过对铝质正六边形蜂窝胞元壳进行模拟,将其结果与公式的计算结果相比,两者非常接近,证实了理论分析的有效性。其结论对蜂窝夹层结构和薄壁棱柱壳的理论研究有重要的指导意义。

关键词: 蜂窝夹层结构, 临界载荷, 屈曲失稳, 数值模拟

Abstract: Taking a cellular shell of regular hexagonal honeyc- omb sandwich as example, the buckling theories of Euler colu- mn and thin-walled plate are combined. The treble series solut- ion of cellular shell buckling mode and the critical loading formulas are derived. The short cellular shell, medium length cellular shell, and the long cellular shell have been classified according to the failure forms of cellar structure. The perfectly designiug theory is builtup and the critical loading chart is pro-vided. It can be found that the different classical cellular shell has different controlling equation and first-order buckling form-ation. Finally the calculated results with derived formulas are coincidence with 3D finite element analysis results. The concl-usions will have significant reference for the study of a honeyc-omb sandwich structure and thin-walled prismatic shell.

Key words: Buckling mode, Critical loading, Honeycomb sandwich structure, Numeric simulation

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