000			01972nam a2200265 a 4500
001			vtls000051474
003			KUKTEM
005			20251114204410.0
008			110224t2010 my da f m 000 0 eng d
020			_aTHE0005868(Local)
039		9	_a201905141025 _baida _c201107132219 _dVLOAD _y201102241037 _zida
040			_aUMP
090			_aTA460 .N39 2010 rs Bc.
100	0		_aMohamad Nazri Ramli
245	1	0	_aFatigue life prediction of aluminium alloy by using finite element analysis / _cMohamad Nazri Ramli
246	3		_aFatigue life prediction of aluminium alloy by using finite element analysis _h[electronic resource]
260			_aKuantan, Pahang : _bUMP, _c2010
300			_axvi, 58 p. : _bill. (some col.) ; _c30 cm. + _e1 computer disc
502			_aProject paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2010
504			_aBibliography : p. 53
520	3		_aThe total fatigue life cycle of aluminium alloys was investigated using finite element analysis. The effect of stress concentration factors on fatigue life was analyzed using pre-post MSC.Patran and MSC.Nastran for stress analysis whereas MSC.Fatigue was used for fatigue analysis. The aluminium alloys was selected for this project since it is typically used to make most of the mechanical components. Six different models with varies stress concentration factors were analyzed. The model used in this study is standard tensile specimens in accordance to the ASTM (American Society for Testing and Materials). The stress amplitude curve, S as a function of number of cycles to failure, N was plotted in order to compute the total life cycles of the models and endurance limit as well. Based on the results, it shows that the model with higher stress concentration factor, Kt have lower life cycles.
650		0	_aMetals _xFatigue
650		0	_aFinite element method
999			_aVIRTUA40 _c1350 _d1356
999			_aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992