01866nam a2200265 a 4500 vtls000052255 KUKTEM 20251114204444.0 110324t2010 my a f m 000 0 eng d THE0005743(Local) 201905221023 hanafiah 201107140040 VLOAD 201103241201 ida UMP TA418.38 .A25 2010 rs Bc. Mohamad Abiddullah Mohd Lasim Finite element based fatigue crack growth of cracked plates under axial loading / Mohamad Abiddullah Mohd Lasim Finite element based fatigue crack growth of cracked plates under axial loading [electronic resource] Kuantan, Pahang : UMP, 2010 xi, 42 p. : ill. (some col.) ; 30 cm.+ 1 computer disc Project paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2010 Bibliography : p. 39-40 This 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). Materials Fatigue Finite element method 0 0 0 1 20000 20000 2019-09-04 0 TA418.38 .A25 2010 rs Bc. 0000053885 2019-09-04 00:00:00 1 2019-09-04 PSM 0 0 0 1 20000 20000 2019-09-04 0 CD 4958 | TA418.38 .A25 2010 rs Bc. 0000053886 2019-09-04 00:00:00 1 2019-09-04 PSM VIRTUA40 2323 2329 VTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992