A FINITE-ELEMENT ANALYSIS OF INPLANE THERMOSTRUCTURAL BEHAVIOR OF COMPOSITE PLATES

被引：11

作者：

MUKHERJEE, N ^{[1
]}

SINHA, PK ^{[1
]}

机构：

[1] INDIAN INST TECHNOL,DEPT AEROSP ENGN,KHARAGPUR 721302,W BENGAL,INDIA

来源：

JOURNAL OF REINFORCED PLASTICS AND COMPOSITES | 1993年 / 12卷 / 10期

关键词：

COMPOSITES; METAL MATRIX; CONDUCTION; TEMPERATURE; DISPLACEMENT; THERMAL STRESS; FINITE ELEMENT;

D O I：

10.1177/073168449301201001

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

A Galerkin finite element procedure is adopted to solve the thermostructural problem for generally anisotropic as well as symmetrically laminated composite plates. The two-dimensional temperature field is first computed and subsequently, the quasi-static inplane response of the structure is evaluated. Both steady and transient states are analysed, taking into account all conventional modes of heat transfer and the temperature dependence of several thermomechanical properties. Nonlinearity has been tackled with the help of the Euler's backward difference procedure in conjunction with a modified Newton-Raphson scheme for convergence.

引用

页码：1026 / 1042

页数：17

共 15 条

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