Investigation of abrasive waterjet peening process on bending strength and erosion resistance of different ply combination of fibre metal laminate based aluminium-lithium alloy / (Record no. 101180)

MARC details
000 -LEADER
fixed length control field 04160ntm a2200337 i 4500
003 - CONTROL NUMBER IDENTIFIER
control field MY-KuUP
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20251125110920.0
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 240823t20242024my a|||fr|||| 000 0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number THE0009934 (Local)
Qualifying information Hardback
040 ## - CATALOGING SOURCE
Original cataloging agency UMPSA
Language of cataloging eng
Transcribing agency UMP
Description conventions rda
090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN)
Classification number (OCLC) (R) ; Classification number, CALL (RLIN) (NR) FTKPM .Q83 2024 r Thesis
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Syed Qutaba Bin Tariq,
Relator term author.
245 10 - TITLE STATEMENT
Title Investigation of abrasive waterjet peening process on bending strength and erosion resistance of different ply combination of fibre metal laminate based aluminium-lithium alloy /
Statement of responsibility, etc. Syed Qutaba Bin Tariq
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 2024
264 #4 - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Date of production, publication, distribution, manufacture, or copyright notice © 2024
300 ## - PHYSICAL DESCRIPTION
Extent xviii, 186 pages :
Other physical details illustration ;
Materials specified 0 cm. +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 Manufacturing & Mechatronics Engineering Technology
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Doctor of Philosophy) -- Universiti Malaysia Pahang – 2024
504 ## - BIBLIOGRAPHY, ETC. NOTE
-- ncludes bibliographical referenceIncludes bibliographical reference
520 3# - SUMMARY, ETC.
Summary, etc. Fibre metal laminate (FML) composites have been used widely in many applications due to its excellent mechanical properties such as high fatigue and impact resistance as well as high bending resistance and strength. However, the current requirement in aircraft industry requires further improvement in terms of bending and erosion resistance. Peening processes have been used as a surface treatment method to improve the FML properties. Still, the shot peening has limitations in the coverage area and the laser shock peening experiences involvement of high rate of heat during the process. Hence, abrasive waterjet (AWJ) peening can be conveniently used with a more comprehensive coverage of the FML surface and less generation of surface temperature. The objective of the present work is to investigate the effect of abrasive waterjet peening process on the bending strength and erosion resistance and its surface microstructural changes of glass fibre aluminium-lithium laminate reinforced epoxy. The effect of different combination of 3/2 and 4/2 aluminium-lithium alloy and glass fibre sheets on physical and mechanical properties was also investigated. Several peening parameters namely hydraulic pressure, p (69, 97 and 117 MPa), abrasive mesh size, a (80, 120 and 160 #), nozzle standoff distance, d (20, 40 and 60 mm) and number of jet passes, n (1 and 2 passes) were selected for the experimentation. In terms of physical properties, it was found that 4/2 plies FML produced a higher density and thickness because more total number of plies. Meanwhile, 3/2 plies FML resulted in a higher fibre volume fraction since it has lesser number of metallic sheets with the same amount of fibre layers. As a result, tensile and bending strength of 3/2 plies FML were found to be higher as compared to 4/2 plies FML. In terms of the effect of AWJ peening parameters, a higher flexural strength (up to 482 MPa) and a lower surface erosion (up to 3.4 mg) were achieved at medium p, higher a, higher d and multiple n. This constitutes about ± 10% improvement from the original specimen without treatment. In terms of surface microstructural changes, results indicated that the fibre layers hindered the deformation of the aluminium-lithium layer thus increasing the compactness by around 5%. Based on the assessment of scanning electron microscope (SEM) images, it was revealed that the aluminium-lithium layer experienced a severe damage especially at a higher impact intensity of peening process with enlarged surface craters. It can be concluded that the AWJ peening process can improve the flexural strength and erosion resistance of glass fibre aluminium-lithium laminate reinforced epoxy which is advantageous for the application in the aircraft industry
610 20 - SUBJECT ADDED ENTRY--CORPORATE NAME
Corporate name or jurisdiction name as entry element Faculty of Manufacturing & Mechatronics 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
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Theses
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 Copy number Price effective from Koha item type
  Not lost Library of Congress Classification   Not for loan UMPLIB PEKAN UMPLIB PEKAN 23/08/2024   FTKPM .Q83 2024 r Thesis T000003223 23/08/2024 1 23/08/2024 Thesis
  Not lost Library of Congress Classification   Final Processing UMPLIB PEKAN UMPLIB PEKAN 23/08/2024   CD13614 T000003224 23/08/2024 1 23/08/2024 Thesis

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