Predicting surface crack growth behaviour for an api 5l x65 gas pipeline using s-version finite element method / (Record no. 102570)

MARC details
000 -LEADER
fixed length control field 03320nam a2200325 i 4500
003 - CONTROL NUMBER IDENTIFIER
control field MY-KuUP
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20251125111043.0
006 - FIXED-LENGTH DATA ELEMENTS--ADDITIONAL MATERIAL CHARACTERISTICS
fixed length control field t||||fr|||| 000 0
007 - PHYSICAL DESCRIPTION FIXED FIELD--GENERAL INFORMATION
fixed length control field ta
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 250522t20252025my a|||fr|||| 000 0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number THE0010090 (Local)
Qualifying information Hardback
040 ## - CATALOGING SOURCE
Original cataloging agency UMPSA
Language of cataloging eng
Transcribing agency UMPSA
Description conventions rda
090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN)
Classification number (OCLC) (R) ; Classification number, CALL (RLIN) (NR) FTKMA .B35 2025 r Thesis
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Nurul Baini Ghazali,
Relator term author.
245 10 - TITLE STATEMENT
Title Predicting surface crack growth behaviour for an api 5l x65 gas pipeline using s-version finite element method /
Statement of responsibility, etc. Nurul Baini Binti Ghazali
264 #1 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Place of production, publication, distribution, manufacture Kuantan, Pahang :
Name of producer, publisher, distributor, manufacturer UMPSA,
Date of production, publication, distribution, manufacture, or copyright notice 2025
264 #4 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Date of production, publication, distribution, manufacture, or copyright notice © 2025
300 ## - PHYSICAL DESCRIPTION
Extent xiv, 133 pages :
Other physical details illustrations (some color) ;
Dimensions 30 cm. +
Accompanying material 1 CD-ROM
336 ## - CONTENT TYPE
Source rdacontent
Content type term text
337 ## - MEDIA TYPE
Source rdamedia
Media type term unmediated
338 ## - CARRIER TYPE
Source rdacarrier
Carrier type term volume
347 ## - DIGITAL FILE CHARACTERISTICS
Source rda
File type text file
Encoding format PDF
500 ## - GENERAL NOTE
General note Faculty of Mechanical and Automotive Engineering Technology
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Master of Science) -- Universiti Malaysia Pahang – 2025
504 ## - BIBLIOGRAPHY, ETC. NOTE
Bibliography, etc. note Includes bibliographical references
520 3# - SUMMARY, ETC.
Summary, etc. The thesis describes the fatigue crack growth (FCG) behaviour of API 5L X65 gas pipeline surface cracks using S-version FEM. API 5L X65 is widely used in oil & gas for transportation of hydrocarbon gas and crude oil from upstream facilities to downstream facilities and end user such as power station, petrochemicals industries, transportation industries and residential. Beside to suit the purpose in term of chemical and mechanical properties, API 5L X65 is cost effective and have better strength compared to other material grade. Nowadays, the major concern of the engineering application is the material failure. Hence, the fatigue crack analysis needs to carry out to determine the fatigue life of a material. This is important as it is involving the human safety and lead to fatality. In this study, a method known as global-local overlay technique was used to predict fatigue behaviour, which involves two separate meshes, one for global (geometry) and one for local (physics) (crack) by using S-version Finite Element Method (S-version FEM). The pre-post program was used to model the FAST global geometry (coarser mesh) so called CentOS programming, which included the material and boundary conditions. As a result, the exact location of the local crack (finer mesh) will be defined, and the mesh control will be adjusted accordingly. The Paris’ crack model is used to predict the fatigue crack behaviour of this material. Local mesh was overlaid with the global mesh before the numerical computation to solve the engineering problem. The virtual crack closure-integral method (VCCM) was used to calculate the stress intensity factors (SIF). The most important result is the fatigue crack growth behaviour, which includes the crack depth (a), crack length (c), and stress intensity factors (SIF). The SIF value is important as it affect the crack growth. Then, the fatigue crack growth with 0.4 aspect ratio (a/c) is determined. After that, different a/c is used to compare the result obtained in S-version FEM with analytical solution in Newman & Raju 1979.
610 20 - SUBJECT ADDED ENTRY--CORPORATE NAME
Corporate name or jurisdiction name as entry element Faculty of Mechanical and Automotive Engineering Technology
General subdivision Dissertations
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Universities and colleges
General subdivision Dissertations
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme Library of Congress Classification
Koha item type Thesis
Holdings
Withdrawn status Lost status Source of classification or shelving scheme Damaged status Not for loan Home library Current library Date acquired Total checkouts Full call number Barcode Date last seen Price effective from Koha item type Copy number Public note
  Not lost Library of Congress Classification   Not for loan UMPLIB PEKAN UMPLIB PEKAN 22/05/2025   FTKMA .B35 2025 r Thesis T000003530 22/05/2025 22/05/2025 Thesis    
  Not lost Library of Congress Classification   Not for loan UMPLIB PEKAN UMPLIB PEKAN 04/06/2025   FTKMA .B35 2025 r Thesis T000003466 04/06/2025 04/06/2025 Thesis 2 c.2

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