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...
Saved in:
Main Authors: | , , |
---|---|
Format: | Conference or Workshop Item |
Language: | English English |
Published: |
2021
|
Subjects: | |
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/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Universiti Islam Antarabangsa Malaysia |
Language: | English English |
id |
my.iium.irep.93539 |
---|---|
record_format |
dspace |
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/ |
_version_ |
1717093018559840256 |