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...

Full description

Saved in:
Bibliographic Details
Main Author: Mazlan, Shahan
Format: Thesis
Language:English
Published: 2020
Subjects:
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/
Tags: Add Tag
No Tags, Be the first to tag this record!