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

The springback phenomena of CFRP after curing process through autoclave manufacturing method results on the out of tolerance for its utilisation in aerospace industry. This paper relates to the measurements of springback for Uni-directional flat laminate as a first steps to the springback study for...

Full description

Bibliographic Details
Main Authors:	Zakaria, Mohd Hafizu, Aminanda, Yulfian, Ahmad Rashidi, Syazwan, Mohamed Shah @ Mat Sah, Mohamed Sallauddin
Format:	Conference or Workshop Item
Language:	English English
Published:	Institute of Physics Publishing 2018
Subjects:	TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/53034/ http://irep.iium.edu.my/53034/ http://irep.iium.edu.my/53034/ http://irep.iium.edu.my/53034/1/53034_Spring-back%20of%20Thick%20Uni-Directional.pdf http://irep.iium.edu.my/53034/2/53034_Spring-back%20of%20Thick%20Uni-Directional_SCOPUS.pdf

id	iium-53034
recordtype	eprints
spelling	iium-530342018-06-26T08:46:03Z http://irep.iium.edu.my/53034/ Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application Zakaria, Mohd Hafizu Aminanda, Yulfian Ahmad Rashidi, Syazwan Mohamed Shah @ Mat Sah, Mohamed Sallauddin TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics The springback phenomena of CFRP after curing process through autoclave manufacturing method results on the out of tolerance for its utilisation in aerospace industry. This paper relates to the measurements of springback for Uni-directional flat laminate as a first steps to the springback study for the real aircraft composite laminate structures. A flat laminate with dimension of 300 mm x 300 mm, 400 mm x 400 mm and 500mm x 500 mm with different number of ply; 20, 24 and 28 are manufactured. The choice of dimension and number of lay-up corresponds to the dimension and lay-up of rib structure. After process, the springbacks are measured using 3D scanner (optical-based three-dimensional) with an accuracy of 42 micrometers to obtain an accurate measurement. The analysis of the effect of dimension and number of ply to the magnitude of springback are presented within the range of specimen studied in this work. Institute of Physics Publishing 2018 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/53034/1/53034_Spring-back%20of%20Thick%20Uni-Directional.pdf application/pdf en http://irep.iium.edu.my/53034/2/53034_Spring-back%20of%20Thick%20Uni-Directional_SCOPUS.pdf Zakaria, Mohd Hafizu and Aminanda, Yulfian and Ahmad Rashidi, Syazwan and Mohamed Shah @ Mat Sah, Mohamed Sallauddin (2018) Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application. In: 5th International Seminar on Aerospace Science and Technology (ISAST 2017), 27th-29th Sept. 2017, Medan, North Sumatra; Indonesia. http://iopscience.iop.org/article/10.1088/1742-6596/1005/1/012003 10.1088/1742-6596/1005/1/012003
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics TL500 Aeronautics Zakaria, Mohd Hafizu Aminanda, Yulfian Ahmad Rashidi, Syazwan Mohamed Shah @ Mat Sah, Mohamed Sallauddin Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
description	The springback phenomena of CFRP after curing process through autoclave manufacturing method results on the out of tolerance for its utilisation in aerospace industry. This paper relates to the measurements of springback for Uni-directional flat laminate as a first steps to the springback study for the real aircraft composite laminate structures. A flat laminate with dimension of 300 mm x 300 mm, 400 mm x 400 mm and 500mm x 500 mm with different number of ply; 20, 24 and 28 are manufactured. The choice of dimension and number of lay-up corresponds to the dimension and lay-up of rib structure. After process, the springbacks are measured using 3D scanner (optical-based three-dimensional) with an accuracy of 42 micrometers to obtain an accurate measurement. The analysis of the effect of dimension and number of ply to the magnitude of springback are presented within the range of specimen studied in this work.
format	Conference or Workshop Item
author	Zakaria, Mohd Hafizu Aminanda, Yulfian Ahmad Rashidi, Syazwan Mohamed Shah @ Mat Sah, Mohamed Sallauddin
author_facet	Zakaria, Mohd Hafizu Aminanda, Yulfian Ahmad Rashidi, Syazwan Mohamed Shah @ Mat Sah, Mohamed Sallauddin
author_sort	Zakaria, Mohd Hafizu
title	Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_short	Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_full	Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_fullStr	Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_full_unstemmed	Spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
title_sort	spring-back of thick uni-directional carbon fibre reinforced composite laminate for aircraft structure application
publisher	Institute of Physics Publishing
publishDate	2018
url	http://irep.iium.edu.my/53034/ http://irep.iium.edu.my/53034/ http://irep.iium.edu.my/53034/ http://irep.iium.edu.my/53034/1/53034_Spring-back%20of%20Thick%20Uni-Directional.pdf http://irep.iium.edu.my/53034/2/53034_Spring-back%20of%20Thick%20Uni-Directional_SCOPUS.pdf
first_indexed	2023-09-18T21:15:06Z
last_indexed	2023-09-18T21:15:06Z
_version_	1777411509228404736

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

Similar Items