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...
محفوظ في:
المؤلف الرئيسي: | Mazlan, Shahan |
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التنسيق: | أطروحة |
اللغة: | English |
منشور في: |
2020
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الموضوعات: | |
الوصول للمادة أونلاين: | http://psasir.upm.edu.my/id/eprint/104170/1/SHAHAN%20BIN%20MAZLAN%20-%20IR.pdf |
الوسوم: |
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