000			02122nam a2200265 a 4500
001			vtls000052261
003			KUKTEM
005			20251114204444.0
008			110324t2010 my a f m 000 0 eng d
020			_aTHE0005749(Local)
039		9	_a201905221038 _bhanafiah _c201107140040 _dVLOAD _y201103241404 _zida
040			_aUMP
090			_aTA418.38 .F83 2010 rs Bc.
100	0		_aFua, Wai Loon
245	1	0	_aFatigue life and crack growth analysis of keyhole specimen / _cFua Wai Loon
246	3		_aFatigue life and crack growth analysis of keyhole specimen _h[electronic resource]
260			_aKuantan, Pahang : _bUMP, _c2010
300			_axiv, 39 p. : _bill. (some col.) ; _c30 cm.+ _e1 computer disc
502			_aProject paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2010
504			_aBibliography : p. [38]-39
520	3		_aThis report deals with the prediction of fatigue life and crack growth for keyhole specimen using variable loading amplitude. The objective of this report is to predict the fatigue life and crack growth of keyhole specimen. The steel such as MANTEN and RQC100 were considered the keyhole materials. The structural three-dimensional solid modeling of keyhole specimen was developed using Solid work. The finite element model and analysis were performed using PATRAN and NASTRAN software. Predicted result is validated with existing experimental result. In addition, the fatigue life was predicted using the strain-life approach subjected to variable amplitude loading. From the results, it is observed that SAETRN loading gives the most conservative results for strain-life method. It is concluded that SAETRN loading history is the most conservative method compared to SAESUS and SAEBKT loading history. RQC100 has a longer crack initiation life but shorter crack propagation life than MANTEN. Apparently, MANTEN more ductile than RQC100. The RQC100 is suitable material of keyhole.
650		0	_aMaterials _xFatigue
650		0	_aFinite element method
999			_aVIRTUA40 _c2340 _d2346
999			_aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992