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...
保存先:
| 第一著者: | |
|---|---|
| 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 |
| 主題: | |
| タグ: |
タグ追加
タグなし, このレコードへの初めてのタグを付けませんか!
|
| 要約: | 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. |
|---|---|
| 記述事項: | Final Year Project |
| 物理的記述: | 1 CD-ROM 4 3/4 in. |