期刊
COMPOSITES SCIENCE AND TECHNOLOGY
卷 71, 期 8, 页码 1089-1097出版社
ELSEVIER SCI LTD
DOI: 10.1016/j.compscitech.2011.03.014
关键词
Carbon nanotubes; Carbon fiber; Epoxy; Fatigue; Polymer-matrix composites(PMCs); Mechanical properties; Resin transfer moulding(RTM); Raman spectroscopy
资金
- NASA [NCC-1-02038]
- University Research Engineering and Technology Institutes (URETIs)
- Air Force Office of Scientific Research, United States
- National Science Foundation NSF [0453578]
- Air Force Research Laboratory Clarkson Aerospace Corporation [FA8650-05-D-1912]
- AFRL [FA8650-05-D-1912]
- Directorate For Engineering
- Div Of Engineering Education and Centers [0453578] Funding Source: National Science Foundation
Carbon fiber reinforced epoxy composite laminates are studied for improvements in quasi static strength and stiffness and tension-tension fatigue cycling at stress-ratio (R-ratio) = +0.1 through strategically incorporating amine functionalized single wall carbon nanotubes (a-SWCNTs) at the fiber/fabric-matrix interfaces over the laminate cross-section. In a comparison to composite laminate material without carbon nanotube reinforcements there are modest improvements in the mechanical properties of strength and stiffness; but, a potentially significant increase is demonstrated for the long-term fatigue life of these functionalized nanotube reinforced composite materials. These results are compared with previous research on the cyclic life of this carbon fiber epoxy composite laminate system reinforced similarly with side wall fluorine functionalized industrial grade carbon nanotubes. Optical and scanning electron microscopy and Raman spectrometry are used to confirm the effectiveness of this strategy for the improvements in strength, stiffness and fatigue life of composite laminate materials using functionalized carbon nanotubes. (C) 2011 Elsevier Ltd. All rights reserved.
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