Analysis of multilayered composite cylinders under thermal loading

被引：22
|
作者：
Akçay, IH
Kaynak, I [1 ]
机构：
[1] Dokuz Eylul Univ, Dept Mech Engn, TR-35100 Izmir, Turkey
[2] Suleyman Demirel Univ, Dept Mech Engn, Isparta, Turkey
来源：
JOURNAL OF REINFORCED PLASTICS AND COMPOSITES | 2005年 / 24卷 / 11期
关键词：
composite pressure vessel; plane-strain case; thermal loading; composite cylinder;
D O I：
10.1177/0731684405048840
中图分类号：
TB33 [复合材料];
学科分类号：
摘要：
In this investigation, a failure analysis is performed on analytical expressions of multilayered filament wound structures (FWS) in composite cylinders for the plane-strain and closed-end condition cases, under internal pressure and uniform thermal loading. The multilayer filament wound composite pressure closed-end cylinders are oriented symmetrically and antisymmetrically. The mechanical properties of composite cylinders are investigated considering a glass-epoxy multilayered composite cylinder. The failure analysis is carried out on different orientations of the multilayered composite cylinders. The failure pressure is found to be high at increased temperatures for the plane-strain cases. It is nearly the same for the closed-end case.
引用
收藏
页码：1169 / 1179
页数：11
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