MODELING OF DELAMINATION BUCKLING IN COMPOSITE CYLINDRICAL-SHELLS WITH A NEW HIGHER-ORDER THEORY

被引：16

作者：

CHATTOPADHYAY, A

GU, HZ

机构：

[1] Department of Mechanical and Aerospace Engineering, Arizona State University, Tempe

来源：

COMPOSITES SCIENCE AND TECHNOLOGY | 1995年 / 54卷 / 02期

关键词：

BUCKLING; COMPOSITES; DELAMINATION; HIGHER-ORDER THEORY; CYLINDRICAL SHELLS;

D O I：

10.1016/0266-3538(95)00054-2

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

A higher-order shear deformation theory has been employed for evaluating accurately the transverse shear effects in delamination buckling of cylindrical shells under axial compression. The governing differential equations of the present theory are obtained by applying the principle of the stationary value of the total potential. The Rayleigh-Ritz method is used to solve the equations by assuming a double Fourier expansion of the displacements with trigonometric coordinate functions. Numerical results for linear delamination buckling of axially compressed cylindrical shells with clamped ends are presented to validate the theory. Comparisons are made with the classical laminate theory and first-order theory results.

引用

页码：223 / 232

页数：10

共 29 条

[1] MODELING OF DELAMINATION IN COMPOSITE LAMINATES USING A LAYER-WISE PLATE-THEORY [J].