The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah.

The attachment of the fin plate of MiG-29 aircraft was inspected by using conventional ultrasonic testing method. Ultrasonic non-destructive testing, also known as ultrasonic NDT or simply UT, is a method of characterizing the thickness or internal structure of a test piece through the use of high f...

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Main Author: Hamzah, Siti Nur Hasanah
Format: Student Project
Language:English
Published: 2013
Subjects:
Online Access:https://ir.uitm.edu.my/id/eprint/45421/1/45421.pdf
https://ir.uitm.edu.my/id/eprint/45421/
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spelling my.uitm.ir.454212022-11-11T07:28:39Z https://ir.uitm.edu.my/id/eprint/45421/ The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah. Hamzah, Siti Nur Hasanah Descriptive and experimental mechanics Electricity and magnetism Aeronautics. Aeronautical engineering The attachment of the fin plate of MiG-29 aircraft was inspected by using conventional ultrasonic testing method. Ultrasonic non-destructive testing, also known as ultrasonic NDT or simply UT, is a method of characterizing the thickness or internal structure of a test piece through the use of high frequency sound waves. The frequencies, or pitch, used for ultrasonic testing are many times higher than the limit of human hearing, most commonly in the range from 500 KHz to 20 MHz. Ultrasonic testing was significant for quality assessment and evaluation of the critical part component in aircraft such as the fins without altering or damaging the material under the test. Pulse echo technique is the most common technique used in ultrasonic testing which make used the phenomenon that sound waves travel in straight line and are reflected by an obstacles placed in their way. The effects of different probes frequency (5MHz, 10 MHz and 20MHz) were observed by analyzing the signal produced from the ultrasonic test set being used. Higher frequency probes have shorter wavelength and this will increase the sensitivity to locate the defect in the test material. Therefore, for a thin material as the fin plate it was recommended to use a higher frequency since it promotes a shorter wavelength into the test material being inspected. Since the type of material and couplant used have severe affects on the testing results, therefore the material and the type of couplant used were kept constant throughout the inspection. Throughout the testing, fin plate made of aluminium alloy D19 and couplant (petroleum grease) were used to ensure the different variables affecting the result of the testing. 2013 Student Project NonPeerReviewed text en https://ir.uitm.edu.my/id/eprint/45421/1/45421.pdf The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah. (2013) [Student Project] (Unpublished)
institution Universiti Teknologi Mara
building Tun Abdul Razak Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Mara
content_source UiTM Institutional Repository
url_provider http://ir.uitm.edu.my/
language English
topic Descriptive and experimental mechanics
Electricity and magnetism
Aeronautics. Aeronautical engineering
spellingShingle Descriptive and experimental mechanics
Electricity and magnetism
Aeronautics. Aeronautical engineering
Hamzah, Siti Nur Hasanah
The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah.
description The attachment of the fin plate of MiG-29 aircraft was inspected by using conventional ultrasonic testing method. Ultrasonic non-destructive testing, also known as ultrasonic NDT or simply UT, is a method of characterizing the thickness or internal structure of a test piece through the use of high frequency sound waves. The frequencies, or pitch, used for ultrasonic testing are many times higher than the limit of human hearing, most commonly in the range from 500 KHz to 20 MHz. Ultrasonic testing was significant for quality assessment and evaluation of the critical part component in aircraft such as the fins without altering or damaging the material under the test. Pulse echo technique is the most common technique used in ultrasonic testing which make used the phenomenon that sound waves travel in straight line and are reflected by an obstacles placed in their way. The effects of different probes frequency (5MHz, 10 MHz and 20MHz) were observed by analyzing the signal produced from the ultrasonic test set being used. Higher frequency probes have shorter wavelength and this will increase the sensitivity to locate the defect in the test material. Therefore, for a thin material as the fin plate it was recommended to use a higher frequency since it promotes a shorter wavelength into the test material being inspected. Since the type of material and couplant used have severe affects on the testing results, therefore the material and the type of couplant used were kept constant throughout the inspection. Throughout the testing, fin plate made of aluminium alloy D19 and couplant (petroleum grease) were used to ensure the different variables affecting the result of the testing.
format Student Project
author Hamzah, Siti Nur Hasanah
author_facet Hamzah, Siti Nur Hasanah
author_sort Hamzah, Siti Nur Hasanah
title The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah.
title_short The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah.
title_full The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah.
title_fullStr The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah.
title_full_unstemmed The investigation of fin plate of MiG-29 aircraft made of aluminium alloy D19 using conventional ultrasonic testing (A-Scan System) / Siti Nur Hasanah Hamzah.
title_sort investigation of fin plate of mig-29 aircraft made of aluminium alloy d19 using conventional ultrasonic testing (a-scan system) / siti nur hasanah hamzah.
publishDate 2013
url https://ir.uitm.edu.my/id/eprint/45421/1/45421.pdf
https://ir.uitm.edu.my/id/eprint/45421/
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score 13.214268