Evaluation of adhesive strength between glass fiber-epoxy composite and aluminium alloy under opening crack mode loading condition
Adhesive joint technology has potential to replace rivet joint on aeroplane, especially for component made of composite. The fact that the composite should not be applied machining process as reported by Changing Wang, 2016 [1] that machining can cause rashes due to delamination in the composite. To...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/22324 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |