Buiding of composite system FPR wing using prepreg
The effect of fibre reinforcement and resin content on moisture uptake in composite laminate was investigated. Three materials using identical epoxy resin systems but different reinforcements glass, kevlar and carbon fibers and immersed in metyl ethyl keton( MEK ) solven were examined. Samples were...
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| フォーマット: | 電子媒体 ソフトウェア データベース |
| 言語: | English |
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| LEADER | 01506nmi a2200241 a 4500 | ||
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| 003 | MY-KaKUK | ||
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| 039 | 9 | |a 201901311250 |b NMN |c 201111291743 |d VLOAD |c 201007291034 |d AYAR |c 200909281118 |d RAR |y 200905131419 |z SNSA | |
| 090 | 0 | 0 | |a TN665 |b B2S623 2008 |
| 100 | 0 | |a Siti Noorkhartina Binti Ishak |e author | |
| 245 | 1 | 0 | |a Buiding of composite system FPR wing using prepreg |h [electronic resource] / |c Siti Noorkhartina Binti Ishak. |
| 264 | 0 | |a Perlis, Malaysia |b School of Materials Engineering, Universiti Malaysia Perlis |c 2008. | |
| 300 | |a 1 CD-ROM |c 4 3/4 in. | ||
| 500 | |a Final Year Project | ||
| 520 | |a The effect of fibre reinforcement and resin content on moisture uptake in composite laminate was investigated. Three materials using identical epoxy resin systems but different reinforcements glass, kevlar and carbon fibers and immersed in metyl ethyl keton( MEK ) solven were examined. Samples were characterized by DSC in terms of percent of resin in prepreg. Mechanical and thermal properties including tensile modulus, tensile strength, and glass transition temperature were measured. | ||
| 650 | 0 | |a Metallurgy. | |
| 949 | |a VIRTUAITEM |d 30000 |f 1 |x 701 |6 902000351 |a TN665 B2S623 2008 | ||
| 942 | |2 lcc |c COMPFILE | ||
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