航空学报 > 1991, Vol. 12 Issue (12): 598-605

复合材料薄壁圆柱壳体的稳定性

王俊奎1, 王虎2   

  1. 1. 北京航空航天大学 ;2. 中国机载设备公司
  • 收稿日期:1989-12-12 修回日期:1990-04-14 出版日期:1991-12-25 发布日期:1991-12-25

STABILITY OF THIN CIRCULAR CYLINDRICAL SHELLS COMPOSED OF COMPOSITE MATERIALS

Wang Junkui1, Wang Hu2   

  1. 1. Beiing University of Aeronautics;
  • Received:1989-12-12 Revised:1990-04-14 Online:1991-12-25 Published:1991-12-25

摘要: 本文讨论了复合材料圆柱壳体稳定性的复杂性,总结了已经取得的研究成果,并与有关实验进行了比较。重点评述了几何非线性、物理非线性、初始缺陷、横向剪切效应和前屈曲变形状态等因素对失稳性能的影响。对今后的工作给出了建议。

关键词: 复合材料, 圆柱壳, 薄壳, 稳定性

Abstract: The complexity of stability of thin circular cylindrical shells composed of composite materials is discussed and a survey is presented. The known theoretical results of the shells subjected to axial compression, external or/and internal pressure, torsion and their combinations are summarized and compared with the experimental ones. The emphasis is placed on the effect of geometrical and physical nonlinearity, initial imperfections, transverse shear deflection and prebuckling state on the buckling behaviour of laminated composite circular cylindrical shells. The dynamic stability, buckling propagation, elastic wave motion and other behaviour of this type shell are also introduced and discussed.At the end of this paper,recommended works for the future are also discussed.

Key words: composite structure, circular cylindrical shell, thin shell, stability