THERMOELASTIC MODEL FOR MULTIDIRECTIONAL COATED-FIBER COMPOSITES - TRACTION FORMULATION

被引:46
作者
PAGANO, NJ
TANDON, GP
机构
[1] WRDC, MLBM, Air Force Wright Aeronautical Laboratories
[2] AdTech Systems Research Inc., Dayton, OH 45432
关键词
D O I
10.1016/0266-3538(90)90061-9
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this work a companion model to that given earlier is developed to approximate the thermoelastic response of a composite body reinforced by coated fibers oriented in various directions. The fundamental representative volume element is a three-phase concentric circular cylinder under prescribed surface tractions which are independent of the axial coordinate. The analysis leads to a lower bound calculation of the effective moduli which, together with the upper bound results, provides a more precise estimate of the overall composite properties. A parametric study has been further conducted to illustrate the effect of different coating materials and thicknesses on the effective properties and micro-stress distribution within the constituents of a three-dimensional fibrous composite subjected to a uniform temperature change. © 1990.
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页码:247 / 269
页数:23
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