An experimental investigation of the properties of cross-ply laminate used for manufacturing of small aircraft components

被引：4
作者：
Epaarachchi, Jayantha A. [1 ]
Clegg, Richard
机构：
[1] Univ Cent Queensland, James Goldston Fac Engn & Phys Syst, Sch Adv Technol & Proc, Rockhampton, Qld 4702, Australia
[2] Univ Cent Queensland, Proc Engn & Light Met Ctr, Gladstone, Qld 4680, Australia
来源：
COMPOSITE STRUCTURES | 2006年 / 75卷 / 1-4期
关键词：
composites; woven roving; mechanical properties; fatigue properties;
D O I：
10.1016/j.compstruct.2006.04.080
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
This paper discusses the observations and results from an experimental investigation of cross ply laminates used to construct major structural components of a small aircraft manufactured in Australia. The static and fatigue experimental results are compared with established models in composites analysis and with the available data in composite databases. An analysis was done to statistically quantify any deviation of actual properties from the calculated values and investigate the differences in designed and actual capacities/operational life of the components made using this laminates. (C) 2006 Elsevier Ltd. All rights reserved.
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收藏
页码：93 / 99
页数：7
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