Epaarachchi, Jayantha A. and Clegg, Richard (2006) An experimental investigation of the properties of cross-ply laminate used for manufacturing of small aircraft components. Composite Structures, 75 (1-4). pp. 93-99. ISSN 0263-8223
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Official URL: http://dx.doi.org/10.1016/j.compstruct.2006.04.080
Identification Number or DOI: doi: 10.1016/j.compstruct.2006.04.080
Abstract
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.
| Item Type: | Article (Commonwealth Reporting Category C) |
|---|---|
| Uncontrolled Keywords: | composites; woven roving; mechanical properties; fatigue properties |
| Fields of Research (FOR2008): | 09 Engineering > 0912 Materials Engineering > 091202 Composite and Hybrid Materials |
| Subjects: | 290000 Engineering and Technology > 291400 Materials Engineering > 291402 Composite Materials |
| Socio-Economic Objective (SEO2008): | UNSPECIFIED |
| ID Code: | 3512 |
| Deposited By: | |
| Deposited On: | 08 Nov 2007 09:15 |
| Last Modified: | 17 Nov 2011 13:58 |
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