000			01866nam a2200265 a 4500
001			vtls000052255
003			KUKTEM
005			20251114204444.0
008			110324t2010 my a f m 000 0 eng d
020			_aTHE0005743(Local)
039		9	_a201905221023 _bhanafiah _c201107140040 _dVLOAD _y201103241201 _zida
040			_aUMP
090			_aTA418.38 .A25 2010 rs Bc.
100	0		_aMohamad Abiddullah Mohd Lasim
245	1	0	_aFinite element based fatigue crack growth of cracked plates under axial loading / _cMohamad Abiddullah Mohd Lasim
246	3		_aFinite element based fatigue crack growth of cracked plates under axial loading _h[electronic resource]
260			_aKuantan, Pahang : _bUMP, _c2010
300			_axi, 42 p. : _bill. (some col.) ; _c30 cm.+ _e1 computer disc
502			_aProject paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2010
504			_aBibliography : p. 39-40
520	3		_aThis project deals with the finite element based crack growth of the plate under axial loading. The structural model of cracked plate is developed using solidworks software. The finite element modelling and analysis of crack plate were performed utilizing the MSC.PATRAN and MSC.NASTRAN software respectively. The linear elastics method is used for crack growth analysis, it can be seen that Tetrahedral 10 chosen to be use for the overall analysis because it the TET10 are able to capture the higher stresses compared to TET4 for the same mesh global length and maximum principal stress with meshing sizes 0.2 mm. For the crack growth analysis, surface crack is the suitable orientation compared to other orientation with given the longer life (cycles).
650		0	_aMaterials _xFatigue
650		0	_aFinite element method
999			_aVIRTUA40 _c2323 _d2329
999			_aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992