Mohd Farhan Han, Syaza Najwa (2017) Fatigue analysis on bonding of aluminium and carbon laminate composite. Project Report. Universiti Teknikal Malaysia Melaka, Melaka, Malaysia. (Submitted)
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Abstract
Adhesive bonding at the structural component has become an alternative method in industries compared to other conventional methods and the adhesive used in this research was made up by the mixture of aluminium powder-epoxy adhesive. In this research, fatigue testing was conducted and analysed the fatigue life on bonding of aluminium and carbon laminate composite. Percentage of stress level influence the fatigue life of single lap joint between aluminium and carbon laminate composite. Experimental results showed that the higher percentage of stress level gives a small number of cycles to failure and the lower percentage of stress level gives a large number of cycles to failure. The fatigue life of single lap joint for 10% stress level is 1 229 323 cycles whereas the average life cycles for 80% stress level is 14 cycles. The type of bond failure can be identified as the specimens fail under the fatigue testing either it is an adhesion failure or cohesion failure.
| Item Type: | Final Year Project (Project Report) |
|---|---|
| Uncontrolled Keywords: | Manufacturing processes, Composite materials - Mechanical properties, Carbon composites |
| Subjects: | T Technology > T Technology (General) T Technology > TA Engineering (General). Civil engineering (General) |
| Divisions: | Library > Final Year Project > FKM |
| Depositing User: | Mohd Hannif Jamaludin |
| Date Deposited: | 21 Dec 2018 06:35 |
| Last Modified: | 25 Apr 2025 08:35 |
| URI: | http://digitalcollection.utem.edu.my/id/eprint/22385 |
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