000 02283ntm a2200265 a 4500
001 vtls000081944
003 KUKTEM
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008 141016t2013 my da f m 000 0 eng d
020 _aTHE0007678(Local)
039 9 _a201905171538
_bfawwaz
_c201411051230
_dsafura
_y201410161119
_zFida
040 _aUMP
090 _aTS227 .L44 2013 r Bc.
100 1 _aLee, Chee Wor
245 1 0 _aStress behaviour of tailor welded blanks for dissimilar metals using finite element method /
_cLee Chee Wor
260 _aKuantan, Pahang :
_bUMP,
_c2013
300 _axv, 61 p. :
_bill. ;
_c30 cm. +
_e1 CD-ROM
502 _aProject paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang – 2013
504 _aBibliography : p.60-61
520 3 _aThis project presents the stress analysis on tailor welded blanks for dissimilar metals using finite element method. The application of the tailor welded blanks in automotive industries has a large potential and the critical location on the tailor welded blanks based on the stress analysis is important. The structural modeling of the tailor welded blanks is developed using computer aided design software. The method used for tailor welded blanks are later welding. The effect of different materials combination and different configuration on tailor welded blanks on welding behavior is another importance of this study. Finite element method is used to investigate the stress on the tailor welded blanks. Goldak’s double ellipsoid source model is used as the heat source model of the investigation. The changes of power in current and voltages, dissimilar metals of aluminium and steel; and the plate-configuration, L-configuration and T-configuration are investigated in this study. The increase of power increases the hot affected zone and distortion of the plate. The heat is dissipated faster at the aluminium plate compared to steel plate makes the stress concentrated at the steel plate. The stress is distributed outside the welding line for the T-configuration due to the fusion process is not complete.
650 0 _aGas metal arc welding
650 0 _aAluminum
650 0 _aMild steel
999 _aVIRTUA40
_c5082
_d5088
999 _aVTLSSORT0080*0200*0400*0900*1000*2450*2600*3000*5020*5040*5200*6500*6501*6502*9992