Optimization of stiffened panel fatigue life by using finite element analysis
Aluminum Al 2024-T351 and titanium Ti–6Al–4V are widely used in aircraft components such as wings, fuselage, steam turbines and heat exchangers are prone to failure due to fatigue. In design, a range of operating temperatures, fluctuating working loads, duration and manufacturing processes are impor...
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| Format: | Thesis |
| Language: | English |
| Published: |
2020
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| Online Access: | http://psasir.upm.edu.my/id/eprint/104170/1/SHAHAN%20BIN%20MAZLAN%20-%20IR.pdf http://psasir.upm.edu.my/id/eprint/104170/ |
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