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...
Saved in:
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 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Analysis of extrusion using the finite element method /
by: Wong, Wei-tze
Published: (1978) -
The reconciled finite element model of riveted joints structure for crash analysis / Nor Munirah Hassin
by: Hassin, Nor Munirah
Published: (2017) -
Finite Element Analysis and Optimization of Closed Die Forging Process for Aluminium Metal Matrix Composites
by: Abdulmawlla, Mohamed A.
Published: (2010) -
Finite element analysis of buckling behaviour of profiled steel sheet wall panel with window and door opening / Izrul Fizal Mohd Bakri
by: Mohd Bakri, Izrul Fizal
Published: (2001) -
Determination of dynamic characteristic of helical gear using finite element analysis and modal testing / Mohd Izzuddin Yusof
by: Yusof, Mohd Izzuddin
Published: (2009)