Crash analysis of aircraft composite fuselage under belly landing

In aviation industry, accidents during landing are more frequent compared to during take-off, climb up and approaching phases. This study aims to analyse the energy absorption of a Boeing 737 fuselage section under crash belly landing. A finite element model of this fuselage section was created and...

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Main Authors: Syed Abd Rahman AlQudsy, Sharifah Nadhirah, Mohamed Ali, Jaffar Syed, Shaik Dawood, Mohd. Sultan Ibrahim
Format: Conference or Workshop Item
Language:English
English
Published: 2021
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Online Access:http://irep.iium.edu.my/93539/9/ICMAAE21-%20pap%20ID%20110%20%20session%207%20page%2012%20technical-sessionschedule.pdf
http://irep.iium.edu.my/93539/10/93539_Crash%20analysis%20of%20aircraft%20composite.pdf
http://irep.iium.edu.my/93539/
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Institution: Universiti Islam Antarabangsa Malaysia
Language: English
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spelling my.iium.irep.935392021-11-11T03:43:00Z http://irep.iium.edu.my/93539/ Crash analysis of aircraft composite fuselage under belly landing Syed Abd Rahman AlQudsy, Sharifah Nadhirah Mohamed Ali, Jaffar Syed Shaik Dawood, Mohd. Sultan Ibrahim TL500 Aeronautics In aviation industry, accidents during landing are more frequent compared to during take-off, climb up and approaching phases. This study aims to analyse the energy absorption of a Boeing 737 fuselage section under crash belly landing. A finite element model of this fuselage section was created and analyzed using LS-Dyna explicit finite element software. The effects of different vertical impact velocities, terrain conditions, and ply orientations on the composite fuselage skin was studied. For the purpose of investigation, the impact velocities used were 7 m/s and 10 m/s while ground and water surface were used to account for different the terrain conditions. Results showed that frames and skin contribute the most in energy absorption while stringers contribute the least. Other than that, higher impact velocity and ground showed higher energy absorption. 2021 Conference or Workshop Item NonPeerReviewed application/pdf en http://irep.iium.edu.my/93539/9/ICMAAE21-%20pap%20ID%20110%20%20session%207%20page%2012%20technical-sessionschedule.pdf application/pdf en http://irep.iium.edu.my/93539/10/93539_Crash%20analysis%20of%20aircraft%20composite.pdf Syed Abd Rahman AlQudsy, Sharifah Nadhirah and Mohamed Ali, Jaffar Syed and Shaik Dawood, Mohd. Sultan Ibrahim (2021) Crash analysis of aircraft composite fuselage under belly landing. In: International Conference on Mechanical, Automotive and Aerospace Engineering (ICMAAE 2021), 22-23 June 2021, Kuala Lumpur, Malaysia. (Unpublished)
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TL500 Aeronautics
spellingShingle TL500 Aeronautics
Syed Abd Rahman AlQudsy, Sharifah Nadhirah
Mohamed Ali, Jaffar Syed
Shaik Dawood, Mohd. Sultan Ibrahim
Crash analysis of aircraft composite fuselage under belly landing
description In aviation industry, accidents during landing are more frequent compared to during take-off, climb up and approaching phases. This study aims to analyse the energy absorption of a Boeing 737 fuselage section under crash belly landing. A finite element model of this fuselage section was created and analyzed using LS-Dyna explicit finite element software. The effects of different vertical impact velocities, terrain conditions, and ply orientations on the composite fuselage skin was studied. For the purpose of investigation, the impact velocities used were 7 m/s and 10 m/s while ground and water surface were used to account for different the terrain conditions. Results showed that frames and skin contribute the most in energy absorption while stringers contribute the least. Other than that, higher impact velocity and ground showed higher energy absorption.
format Conference or Workshop Item
author Syed Abd Rahman AlQudsy, Sharifah Nadhirah
Mohamed Ali, Jaffar Syed
Shaik Dawood, Mohd. Sultan Ibrahim
author_facet Syed Abd Rahman AlQudsy, Sharifah Nadhirah
Mohamed Ali, Jaffar Syed
Shaik Dawood, Mohd. Sultan Ibrahim
author_sort Syed Abd Rahman AlQudsy, Sharifah Nadhirah
title Crash analysis of aircraft composite fuselage under belly landing
title_short Crash analysis of aircraft composite fuselage under belly landing
title_full Crash analysis of aircraft composite fuselage under belly landing
title_fullStr Crash analysis of aircraft composite fuselage under belly landing
title_full_unstemmed Crash analysis of aircraft composite fuselage under belly landing
title_sort crash analysis of aircraft composite fuselage under belly landing
publishDate 2021
url http://irep.iium.edu.my/93539/9/ICMAAE21-%20pap%20ID%20110%20%20session%207%20page%2012%20technical-sessionschedule.pdf
http://irep.iium.edu.my/93539/10/93539_Crash%20analysis%20of%20aircraft%20composite.pdf
http://irep.iium.edu.my/93539/
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