EXACT SOLUTIONS FOR COMPOSITE LAMINATES IN CYLINDRICAL BENDING

被引：940

作者：

PAGANO, NJ

机构：

[1] Air Force Materials Laboratory, Nonmetallic Materials Division, Wright-Patterson AFB, Washington University, Ohio, St. Louis, Mo.

来源：

JOURNAL OF COMPOSITE MATERIALS | 1969年 / 3卷

关键词：

D O I：

10.1177/002199836900300304

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

Limitations of classical laminated plate theory are investigated by comparing solutions of several specific boundary value problems in this theory to the corresponding theory of elasticity solutions. The general class of problems treated involves the geometric configuration of any number of isotropic or orthotropic layers bonded together and subjected to cylindrical bending. In general it is found that conventional plate theory leads to a very poor description of laminate response at low span-to-depth ratios, but converges to the exact solution as this ratio increases. The analysis presented is also valid in the study of sand wich plates under cylindrical bending. © 1969, Sage Publications. All rights reserved.

引用

页码：398 / &