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Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft

This review-cum-research paper reports the effects of temperature and time exposure on the material behavior of the aerospace aluminum alloys currently in use in subsonic and supersonic aircraft. The research reported in this paper involves experimental study of the microstructural characterization...

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Main Authors: Huda, Z., Zaharinie, T., Min, G.J.
Format: Article
Published: American Society of Civil Engineers 2010
Subjects:
T Technology (General)
Online Access:http://eprints.um.edu.my/14899/
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spelling my.um.eprints.148992015-11-30T02:50:29Z http://eprints.um.edu.my/14899/ Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft Huda, Z. Zaharinie, T. Min, G.J. T Technology (General) This review-cum-research paper reports the effects of temperature and time exposure on the material behavior of the aerospace aluminum alloys currently in use in subsonic and supersonic aircraft. The research reported in this paper involves experimental study of the microstructural characterization and temperature effects on the hardness behavior of the age-hardenable 2024-T3 aluminum alloy; the latter was acquired by one of the authors from Royal Malaysian Air Force (RMAF) aerospace industry. The ALCLAD 2024-T3 alloy is being used in C-130 Hercules aircraft by the RMAF. Recent research on various aluminum alloys being used and being considered for application in Concorde is also reviewed. American Society of Civil Engineers 2010 Article PeerReviewed Huda, Z. and Zaharinie, T. and Min, G.J. (2010) Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft. Journal of Aerospace Engineering, 23 (2). pp. 124-128.
institution Universiti Malaya
building UM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Malaya
content_source UM Research Repository
url_provider http://eprints.um.edu.my/
topic T Technology (General)
spellingShingle T Technology (General)
Huda, Z.
Zaharinie, T.
Min, G.J.
Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft
description This review-cum-research paper reports the effects of temperature and time exposure on the material behavior of the aerospace aluminum alloys currently in use in subsonic and supersonic aircraft. The research reported in this paper involves experimental study of the microstructural characterization and temperature effects on the hardness behavior of the age-hardenable 2024-T3 aluminum alloy; the latter was acquired by one of the authors from Royal Malaysian Air Force (RMAF) aerospace industry. The ALCLAD 2024-T3 alloy is being used in C-130 Hercules aircraft by the RMAF. Recent research on various aluminum alloys being used and being considered for application in Concorde is also reviewed.
format Article
author Huda, Z.
Zaharinie, T.
Min, G.J.
author_facet Huda, Z.
Zaharinie, T.
Min, G.J.
author_sort Huda, Z.
title Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft
title_short Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft
title_full Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft
title_fullStr Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft
title_full_unstemmed Temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft
title_sort temperature effects on material behavior of aerospace aluminum alloys for subsonic and supersonic aircraft
publisher American Society of Civil Engineers
publishDate 2010
url http://eprints.um.edu.my/14899/
_version_ 1643689929069297664
score 13.211869

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