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Finite element based fatigue crack growth of cracked plates under axial loading / Mohamad Abiddullah Mohd Lasim

By:

Mohamad Abiddullah Mohd Lasim

Material type: Text

TextPublication details: Kuantan, Pahang : UMP, 2010Description: xi, 42 p. : ill. (some col.) ; 30 cm.+ 1 computer discISBN:

THE0005743(Local)

Other title:

Finite element based fatigue crack growth of cracked plates under axial loading [electronic resource]

Subject(s):

Dissertation note: Project paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2010 Abstract: 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).

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Holdings ( 2 )
Title notes ( 3 )

Holdings
Item type	Current library	Call number	Copy number	Status	Date due	Barcode
Final Year Report	UMPLIB PEKAN	TA418.38 .A25 2010 rs Bc. (Browse shelf(Opens below))	1	Not for loan		0000053885
Final Year Report	UMPLIB PEKAN	CD 4958 \| TA418.38 .A25 2010 rs Bc. (Browse shelf(Opens below))	1	Not for loan		0000053886

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).