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复合材料薄壁圆柱壳体的稳定性
引用本文:王俊奎,王虎.复合材料薄壁圆柱壳体的稳定性[J].航空学报,1991,12(12):598-605.
作者姓名:王俊奎  王虎
作者单位:北京航空航天大学 (王俊奎),中国机载设备公司(王虎)
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  

STABILITY OF THIN CIRCULAR CYLINDRICAL SHELLS COMPOSED OF COMPOSITE MATERIALS
Beiing University of Aeronautics and AstronauticsWang Tsunkuei.STABILITY OF THIN CIRCULAR CYLINDRICAL SHELLS COMPOSED OF COMPOSITE MATERIALS[J].Acta Aeronautica et Astronautica Sinica,1991,12(12):598-605.
Authors:Beiing University of Aeronautics and AstronauticsWang Tsunkuei
Institution:Wang Junkui
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.
Keywords:composite structure  circular cylindrical shell  thin shell  stability
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