Effects of Interlaminar Morphology on the Fracture Toughness of Carbon Fiber/Epoxy Laminated Composites
碩士 === 國立成功大學 === 化學工程研究所 === 83 === Composite materials often fail by delamination. In this study, two thermoplastic polymers, poly(ether imide) (PEI) and poly( hydroxy ether of bisphenol A) (PHENOXY) were used as particulate interlaminar...
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ndltd-TW-083NCKU00630072015-10-13T12:53:32Z http://ndltd.ncl.edu.tw/handle/54696773728934791894 Effects of Interlaminar Morphology on the Fracture Toughness of Carbon Fiber/Epoxy Laminated Composites 層間微觀形態對(連續碳纖/環氧樹脂)單向複材之耐破壞韌性影響 Kuo-Liang Mao 毛國亮 碩士 國立成功大學 化學工程研究所 83 Composite materials often fail by delamination. In this study, two thermoplastic polymers, poly(ether imide) (PEI) and poly( hydroxy ether of bisphenol A) (PHENOXY) were used as particulate interlaminar toughening agents in graphite/epoxy system. Mode-I and Mode-II delamination toughness was characterized using the Mode-I double-cantilever beam (DCB) and the Mode-II end-notched flexure (ENF) test specimens. The delamination surface was examined by a scanning electron microscope (SEM) to investigate the morphology and fracture mechanism. The results revealed that as the PEI contents were increased, GIC and GIIC increased. GIC was improved from 167 to 527J/m2 at 1mm/min crosshead rate and GIC was improved from 146 to 493J/m2 at a higher crosshead rate of 10mm/min. GIIC improved from 293 to 1297J/m2. In PHENOXY interlaminar toughened system, GIC was almost the same as PEI toughened system, but GIIC was much lower. The fracture surfaces of PEI toughened system showed phase-inversed morphology, and the toughening mechanism was ductile yielding of PEI. Professor Eamor M. Woo 吳逸謨 1995 學位論文 ; thesis 73 zh-TW |
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zh-TW |
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Others
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碩士 === 國立成功大學 === 化學工程研究所 === 83 === Composite materials often fail by delamination. In this study,
two thermoplastic polymers, poly(ether imide) (PEI) and poly(
hydroxy ether of bisphenol A) (PHENOXY) were used as
particulate interlaminar toughening agents in graphite/epoxy
system. Mode-I and Mode-II delamination toughness was
characterized using the Mode-I double-cantilever beam (DCB) and
the Mode-II end-notched flexure (ENF) test specimens. The
delamination surface was examined by a scanning electron
microscope (SEM) to investigate the morphology and fracture
mechanism. The results revealed that as the PEI contents were
increased, GIC and GIIC increased. GIC was improved from 167 to
527J/m2 at 1mm/min crosshead rate and GIC was improved from 146
to 493J/m2 at a higher crosshead rate of 10mm/min. GIIC
improved from 293 to 1297J/m2. In PHENOXY interlaminar
toughened system, GIC was almost the same as PEI toughened
system, but GIIC was much lower. The fracture surfaces of PEI
toughened system showed phase-inversed morphology, and the
toughening mechanism was ductile yielding of PEI.
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author2 |
Professor Eamor M. Woo |
author_facet |
Professor Eamor M. Woo Kuo-Liang Mao 毛國亮 |
author |
Kuo-Liang Mao 毛國亮 |
spellingShingle |
Kuo-Liang Mao 毛國亮 Effects of Interlaminar Morphology on the Fracture Toughness of Carbon Fiber/Epoxy Laminated Composites |
author_sort |
Kuo-Liang Mao |
title |
Effects of Interlaminar Morphology on the Fracture Toughness of Carbon Fiber/Epoxy Laminated Composites |
title_short |
Effects of Interlaminar Morphology on the Fracture Toughness of Carbon Fiber/Epoxy Laminated Composites |
title_full |
Effects of Interlaminar Morphology on the Fracture Toughness of Carbon Fiber/Epoxy Laminated Composites |
title_fullStr |
Effects of Interlaminar Morphology on the Fracture Toughness of Carbon Fiber/Epoxy Laminated Composites |
title_full_unstemmed |
Effects of Interlaminar Morphology on the Fracture Toughness of Carbon Fiber/Epoxy Laminated Composites |
title_sort |
effects of interlaminar morphology on the fracture toughness of carbon fiber/epoxy laminated composites |
publishDate |
1995 |
url |
http://ndltd.ncl.edu.tw/handle/54696773728934791894 |
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