CALCULATION OF STRESSES AT SKIN STIFFENER INTERFACES OF COMPOSITE STIFFENED PANELS UNDER SHEAR LOADS

被引：4
作者：
KASSAPOGLOU, C
机构：
[1] Structures Research Section, Sikorsky Aircraft Division (UTC), Stratford, CT 06601
来源：
INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES | 1993年 / 30卷 / 11期
关键词：
D O I：
10.1016/0020-7683(93)90073-G
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
A simple energy-based approach to calculate stresses at skin-stiffener interfaces of composite stiffened panels under shear loads is presented. Solutions to the governing partial differential equations are sought that satisfy boundary conditions and traction continuity. The stress functional forms are determined by minimizing the energy using a variational approach. The resulting closed form stress expressions are compared to finite element solutions and are shown to be in very good agreement.
引用
收藏
页码：1491 / 1501
页数：11
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