ANALYSIS OF ANISOTROPIC LAMINATED CYLINDRICAL-SHELLS SUBJECTED TO DESTABILIZING LOADS .2. NUMERICAL RESULTS

被引：35

作者：

HAN, BK

SIMITSES, GJ

机构：

[1] Department of Mechanical Engineering, Hong-Ik University, Seoul

[2] Department of Aerospace Engineering and Engineering Mechanics, University of Cincinnati, Cincinnati

来源：

COMPOSITE STRUCTURES | 1991年 / 19卷 / 02期

关键词：

D O I：

10.1016/0263-8223(91)90022-Q

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

In this part, the extensive parametric studies performed are reported and numerical results are presented for the following load cases: lateral pressure, hydrostatic pressure and uniform axial compression. Moreover, a few test cases were considered. These cases were only used for comparison purposes in order to establish the confidence factor of the developed solution methodology. The parameters considered include length to radius ratio, radius to total thickness ratio, stacking sequence and number of plies.

引用

页码：183 / 205

页数：23

共 4 条

[1]

Hess, Stability of orthotropic cylindrical shells under combined loading, J. Am. Rocket Soc., 31, 2, pp. 237-243, (1961)

[2]

Simitses, Shaw, Sheinman, Stability of cylindrical shells by various nonlinear shell theories, Z. Angew. Math. u. Mech. (ZAMM), 65, 3, pp. 159-166, (1985)

[3]

Simitses, Chen, Delamination buckling of pressure-loaded cross-ply laminated cylindrical shells, ZAMM - Journal of Applied Mathematics and Mechanics / Zeitschrift für Angewandte Mathematik und Mechanik, 68, 10, pp. 491-502, (1988)

[4]

Yamaki, Elastic Stability of Circular Cylindrical Shells, (1984)

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