Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application

Spring-back phenomena of a CFRP part takes place after it has gone through a high temperature cure cycle inside an autoclave. These phenomena have caused quality concerns for aerospace part manufacturers due to the part being out-of-tolerance for surface profile. This paper presents the results of t...

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Main Authors:	Zakaria, Mushab, Shaik Dawood, Mohd. Sultan Ibrahim, Aminanda, Yulfian, Ahmad Rashidi, Syazwan, Mat Sah, Mohd Azizi
Format:	Article
Language:	English English
Published:	Blue Eyes Intelligence Engineering and Sciences Publication 2019
Subjects:	T175 Industrial research. Research and development
Online Access:	http://irep.iium.edu.my/72586/ http://irep.iium.edu.my/72586/ http://irep.iium.edu.my/72586/1/72586_Spring%20back%20of%20thick%20curved%20uni-directional.pdf http://irep.iium.edu.my/72586/2/72586_Spring%20back%20of%20thick%20curved%20uni-directional_SCOPUS.pdf

id	iium-72586
recordtype	eprints
spelling	iium-725862019-06-13T06:07:29Z http://irep.iium.edu.my/72586/ Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application Zakaria, Mushab Shaik Dawood, Mohd. Sultan Ibrahim Aminanda, Yulfian Ahmad Rashidi, Syazwan Mat Sah, Mohd Azizi T175 Industrial research. Research and development Spring-back phenomena of a CFRP part takes place after it has gone through a high temperature cure cycle inside an autoclave. These phenomena have caused quality concerns for aerospace part manufacturers due to the part being out-of-tolerance for surface profile. This paper presents the results of the measurement and analysis of thick curved laminates, which are representative of the actual aircraft parts such as the main ribs of an outboard flap. It is a continuation from the previous work with results for flat uni-directional laminates. Curved laminates with sizes of 300mm, 400mm, and 500mm, corner angles of 30°, 45°, and 90°, and thicknesses of 20, 24, and 28 layers were manufactured. The spring-back effect was measured using a 3D scanner to obtain accurate measurements. Within the range of specimen studied in this work, the spring-back value increases with an increment in size. However, for the remaining two factors (thickness and corner angle), the value decreases. Blue Eyes Intelligence Engineering and Sciences Publication 2019-03 Article PeerReviewed application/pdf en http://irep.iium.edu.my/72586/1/72586_Spring%20back%20of%20thick%20curved%20uni-directional.pdf application/pdf en http://irep.iium.edu.my/72586/2/72586_Spring%20back%20of%20thick%20curved%20uni-directional_SCOPUS.pdf Zakaria, Mushab and Shaik Dawood, Mohd. Sultan Ibrahim and Aminanda, Yulfian and Ahmad Rashidi, Syazwan and Mat Sah, Mohd Azizi (2019) Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application. International Journal of Recent Technology and Engineering (IJRTE), 7 (6S). pp. 224-228. ISSN 2277-3878 https://www.ijrte.org/wp-content/uploads/papers/v7i6s/F02440376S19.pdf
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	T175 Industrial research. Research and development
spellingShingle	T175 Industrial research. Research and development Zakaria, Mushab Shaik Dawood, Mohd. Sultan Ibrahim Aminanda, Yulfian Ahmad Rashidi, Syazwan Mat Sah, Mohd Azizi Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application
description	Spring-back phenomena of a CFRP part takes place after it has gone through a high temperature cure cycle inside an autoclave. These phenomena have caused quality concerns for aerospace part manufacturers due to the part being out-of-tolerance for surface profile. This paper presents the results of the measurement and analysis of thick curved laminates, which are representative of the actual aircraft parts such as the main ribs of an outboard flap. It is a continuation from the previous work with results for flat uni-directional laminates. Curved laminates with sizes of 300mm, 400mm, and 500mm, corner angles of 30°, 45°, and 90°, and thicknesses of 20, 24, and 28 layers were manufactured. The spring-back effect was measured using a 3D scanner to obtain accurate measurements. Within the range of specimen studied in this work, the spring-back value increases with an increment in size. However, for the remaining two factors (thickness and corner angle), the value decreases.
format	Article
author	Zakaria, Mushab Shaik Dawood, Mohd. Sultan Ibrahim Aminanda, Yulfian Ahmad Rashidi, Syazwan Mat Sah, Mohd Azizi
author_facet	Zakaria, Mushab Shaik Dawood, Mohd. Sultan Ibrahim Aminanda, Yulfian Ahmad Rashidi, Syazwan Mat Sah, Mohd Azizi
author_sort	Zakaria, Mushab
title	Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_short	Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_full	Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_fullStr	Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_full_unstemmed	Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_sort	spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application
publisher	Blue Eyes Intelligence Engineering and Sciences Publication
publishDate	2019
url	http://irep.iium.edu.my/72586/ http://irep.iium.edu.my/72586/ http://irep.iium.edu.my/72586/1/72586_Spring%20back%20of%20thick%20curved%20uni-directional.pdf http://irep.iium.edu.my/72586/2/72586_Spring%20back%20of%20thick%20curved%20uni-directional_SCOPUS.pdf
first_indexed	2023-09-18T21:42:51Z
last_indexed	2023-09-18T21:42:51Z
_version_	1777413255277314048

Spring back of thick curved uni-directional carbon fibre reinforced composite laminate for aircraft structure application

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