Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis

This paper investigates the compression properties of square honeycomb core materials based on glass fibre reinforced plastic. The objective of this project is to determine the failure strength and energy absorption of the square honeycomb structure and compare both crushing behaviours between the e...

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Main Authors:	Zahidah, Ansari, Tan, Cheng Wen, M. R. M., Rejab, Bachtiar, Dandi, Siregar, J. P., Mohd Zuhri, Mohd Yusuf, Nor Syaza Dinie, Mohd Marzuki
Format:	Article
Language:	English
Published:	Penerbit UMP 2017
Subjects:	TJ Mechanical engineering and machinery
Online Access:	http://umpir.ump.edu.my/id/eprint/19965/ http://umpir.ump.edu.my/id/eprint/19965/ http://umpir.ump.edu.my/id/eprint/19965/ http://umpir.ump.edu.my/id/eprint/19965/1/JMES_Ansari%20et%20al.pdf

id	ump-19965
recordtype	eprints
spelling	ump-199652018-01-11T06:33:02Z http://umpir.ump.edu.my/id/eprint/19965/ Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis Zahidah, Ansari Tan, Cheng Wen M. R. M., Rejab Bachtiar, Dandi Siregar, J. P. Mohd Zuhri, Mohd Yusuf Nor Syaza Dinie, Mohd Marzuki TJ Mechanical engineering and machinery This paper investigates the compression properties of square honeycomb core materials based on glass fibre reinforced plastic. The objective of this project is to determine the failure strength and energy absorption of the square honeycomb structure and compare both crushing behaviours between the experimental and finite element simulations. Control specimen made from GFRP is prepared by using traditional hand lay-up technique and the mechanical properties are determined from the INSTRON Tensile Machine. In this study, the numerical simulation of the square honeycomb structure is analysed with the commercial software. In this simulation, the result obtained for maximum stress is 28.24MPa which is located at node 110451. Besides that, the energy absorption for finite element result and experimental result are 310.86 kJ and 282.17 kJ, respectively. The percentage of error is 9.23% which can be considered a good agreement between numerical simulation and experimental result. Lastly, the crushing behaviour between the finite element model and experimental model is slightly different to each other since the model in simulation is assumed to be the preferred structure, whereas the experimental model is imperfect in the geometric model. Penerbit UMP 2017 Article PeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/19965/1/JMES_Ansari%20et%20al.pdf Zahidah, Ansari and Tan, Cheng Wen and M. R. M., Rejab and Bachtiar, Dandi and Siregar, J. P. and Mohd Zuhri, Mohd Yusuf and Nor Syaza Dinie, Mohd Marzuki (2017) Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis. Journal of Mechanical Engineering and Sciences (JMES) , 11 (2). pp. 2637-2649. ISSN 2289-4659 (print); 2231-8380 (online) https://doi.org/10.15282/jmes.11.2.2017.7.0241 doi: 10.15282/jmes.11.2.2017.7.0241
repository_type	Digital Repository
institution_category	Local University
institution	Universiti Malaysia Pahang
building	UMP Institutional Repository
collection	Online Access
language	English
topic	TJ Mechanical engineering and machinery
spellingShingle	TJ Mechanical engineering and machinery Zahidah, Ansari Tan, Cheng Wen M. R. M., Rejab Bachtiar, Dandi Siregar, J. P. Mohd Zuhri, Mohd Yusuf Nor Syaza Dinie, Mohd Marzuki Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis
description	This paper investigates the compression properties of square honeycomb core materials based on glass fibre reinforced plastic. The objective of this project is to determine the failure strength and energy absorption of the square honeycomb structure and compare both crushing behaviours between the experimental and finite element simulations. Control specimen made from GFRP is prepared by using traditional hand lay-up technique and the mechanical properties are determined from the INSTRON Tensile Machine. In this study, the numerical simulation of the square honeycomb structure is analysed with the commercial software. In this simulation, the result obtained for maximum stress is 28.24MPa which is located at node 110451. Besides that, the energy absorption for finite element result and experimental result are 310.86 kJ and 282.17 kJ, respectively. The percentage of error is 9.23% which can be considered a good agreement between numerical simulation and experimental result. Lastly, the crushing behaviour between the finite element model and experimental model is slightly different to each other since the model in simulation is assumed to be the preferred structure, whereas the experimental model is imperfect in the geometric model.
format	Article
author	Zahidah, Ansari Tan, Cheng Wen M. R. M., Rejab Bachtiar, Dandi Siregar, J. P. Mohd Zuhri, Mohd Yusuf Nor Syaza Dinie, Mohd Marzuki
author_facet	Zahidah, Ansari Tan, Cheng Wen M. R. M., Rejab Bachtiar, Dandi Siregar, J. P. Mohd Zuhri, Mohd Yusuf Nor Syaza Dinie, Mohd Marzuki
author_sort	Zahidah, Ansari
title	Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis
title_short	Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis
title_full	Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis
title_fullStr	Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis
title_full_unstemmed	Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis
title_sort	crushing behaviour of composite square honeycomb structure: a finite element analysis
publisher	Penerbit UMP
publishDate	2017
url	http://umpir.ump.edu.my/id/eprint/19965/ http://umpir.ump.edu.my/id/eprint/19965/ http://umpir.ump.edu.my/id/eprint/19965/ http://umpir.ump.edu.my/id/eprint/19965/1/JMES_Ansari%20et%20al.pdf
first_indexed	2023-09-18T22:28:37Z
last_indexed	2023-09-18T22:28:37Z
_version_	1777416135177666560

Crushing Behaviour of Composite Square Honeycomb Structure: A Finite Element Analysis

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