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Conference Paper: Effect of thermal-cold cycling on properties of glass fiber/ epoxy resin composite for wind turbin blade
Title | Effect of thermal-cold cycling on properties of glass fiber/ epoxy resin composite for wind turbin blade |
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Authors | |
Keywords | Mechanical properties GF/EP composite Epoxy resin Weight loss rate Thermal ageing |
Issue Date | 2012 |
Citation | Advanced Materials Research, 2012, v. 482-484, p. 1483-1489 How to Cite? |
Abstract | The weight loss rate, FTIR characteristic, static mechanical properties and dynamic mecha nical properties of neat epoxy resin and glass fiber/ epoxy resin laminates (GF/EP) after thermal-col d cycling were studied in this paper. The rule of static tensile and flexural strength of neat epoxy resi n and GF/EP after ageing was investigated through the static mechanical properties analysis. The age ing mechanism of GF/EP was studied by analyzing the storage modulus (E'), loss modulus (E"), loss factor of GF/EP and FITR of epoxy resin. The results show that the weight loss rate increases with t he ageing time, which is up to 9% after 400 times ageing cycle. The strength and flexural strength of GF/EP decreased by 6% and 21% after ageing, while the tensile strength of neat epoxy resin incre ases by 8% and its flexural strength increases slightly after ageing. The mechanism analysis reveals t hat internal defects of GF/EP would be induced by thermal-cold cycling stress, which results in the i nterface bonding strength dropping and the performance reducing. © (2012) Trans Tech Publications, Switzerland. |
Persistent Identifier | http://hdl.handle.net/10722/265476 |
ISSN | |
ISI Accession Number ID |
DC Field | Value | Language |
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dc.contributor.author | Tang, Xian He | - |
dc.contributor.author | Lu, Min | - |
dc.contributor.author | Feng, Xue Bin | - |
dc.contributor.author | Liu, Kui | - |
dc.date.accessioned | 2018-12-03T01:20:46Z | - |
dc.date.available | 2018-12-03T01:20:46Z | - |
dc.date.issued | 2012 | - |
dc.identifier.citation | Advanced Materials Research, 2012, v. 482-484, p. 1483-1489 | - |
dc.identifier.issn | 1022-6680 | - |
dc.identifier.uri | http://hdl.handle.net/10722/265476 | - |
dc.description.abstract | The weight loss rate, FTIR characteristic, static mechanical properties and dynamic mecha nical properties of neat epoxy resin and glass fiber/ epoxy resin laminates (GF/EP) after thermal-col d cycling were studied in this paper. The rule of static tensile and flexural strength of neat epoxy resi n and GF/EP after ageing was investigated through the static mechanical properties analysis. The age ing mechanism of GF/EP was studied by analyzing the storage modulus (E'), loss modulus (E"), loss factor of GF/EP and FITR of epoxy resin. The results show that the weight loss rate increases with t he ageing time, which is up to 9% after 400 times ageing cycle. The strength and flexural strength of GF/EP decreased by 6% and 21% after ageing, while the tensile strength of neat epoxy resin incre ases by 8% and its flexural strength increases slightly after ageing. The mechanism analysis reveals t hat internal defects of GF/EP would be induced by thermal-cold cycling stress, which results in the i nterface bonding strength dropping and the performance reducing. © (2012) Trans Tech Publications, Switzerland. | - |
dc.language | eng | - |
dc.relation.ispartof | Advanced Materials Research | - |
dc.subject | Mechanical properties | - |
dc.subject | GF/EP composite | - |
dc.subject | Epoxy resin | - |
dc.subject | Weight loss rate | - |
dc.subject | Thermal ageing | - |
dc.title | Effect of thermal-cold cycling on properties of glass fiber/ epoxy resin composite for wind turbin blade | - |
dc.type | Conference_Paper | - |
dc.description.nature | link_to_subscribed_fulltext | - |
dc.identifier.doi | 10.4028/www.scientific.net/AMR.482-484.1483 | - |
dc.identifier.scopus | eid_2-s2.0-84859207961 | - |
dc.identifier.volume | 482-484 | - |
dc.identifier.spage | 1483 | - |
dc.identifier.epage | 1489 | - |
dc.identifier.isi | WOS:000311059600308 | - |
dc.identifier.issnl | 1022-6680 | - |