摘要
本文以变厚度圆柱壳微分单元为分析模型,导出了拉压不同弹性模量复合材料变厚度圆柱壳弯曲问题的平衡微分方程及其关系式。该方程的COLSYS数值解与ANSYS有限元结果比较表明,本文理论公式正确,基本假定合理,可作为复合材料变厚度圆柱壳较为精确的弯曲理论。
Based on the cylindrical shell element with non-uniform thickness, the equilibrium differential equations of the cylindrical shell with non-uniform thickness and different extension-compressive modulus have been educed. The correctness and efficiency of the present theory is demonstrated by comparison between the COLSYS numerical solutions of the present theory and FEM solutions. The present theory can be taken as the precise theory for the cylindrical shell with non-uniform thickness
出处
《玻璃钢/复合材料》
CAS
CSCD
北大核心
2005年第6期3-6,30,共5页
Fiber Reinforced Plastics/Composites
关键词
复合材料变厚度圆柱壳
拉压不同弹性模量
基本方程
弯曲理论
composite material
non-uniform thickness cylindrical shell
different extension-compression modulus
bending theory
basic equations