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Structural health monitoring (SHM) on high stress loading of wing bracket

This paper presents a Structural Health Monitoring (SHM) approach by addressing the modeling based on Cessna 310 wing bracket to collect its baseline data. SHM is a novel technology application in most engineering field including aircraft and aerospace field for defect detection including crack...

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Main Authors: Imran, Mohd. Salleh, Sarip, Shamsul, Muhtazaruddin, Mohd. Nabil, Hassan, Mohamad Zaki, Md. Daud, Mohd. Yusof, Abdul Aziz, Sa'ardin
Format: Article
Published: AKADEMIA BARU 2016
Subjects:
TL Motor vehicles. Aeronautics. Astronautics
Online Access:http://eprints.utm.my/id/eprint/68433/
http://www.myjurnal.my/public//article-view.php?id=103782
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spelling my.utm.684332017-11-20T08:52:05Z http://eprints.utm.my/id/eprint/68433/ Structural health monitoring (SHM) on high stress loading of wing bracket Imran, Mohd. Salleh Sarip, Shamsul Muhtazaruddin, Mohd. Nabil Hassan, Mohamad Zaki Md. Daud, Mohd. Yusof Abdul Aziz, Sa'ardin TL Motor vehicles. Aeronautics. Astronautics This paper presents a Structural Health Monitoring (SHM) approach by addressing the modeling based on Cessna 310 wing bracket to collect its baseline data. SHM is a novel technology application in most engineering field including aircraft and aerospace field for defect detection including crack and other damage area. The main purpose of this project is to assess their structural integrity due to designated loading and boundary conditions using ABAQUS modeling technique application. These parts were selected as its structures are specifically complex and considered as ageing aircraft parts. The work can be also regarded as platform for CAD model database for ageing aircraft parts investigation upon their structural analyses and design preference. The works begins with a precise measurement using basic gauges and transfer to a 3-D solid modeling using CATIA V6. The optimization technique introduces in this work will be of a novel approach since the CATIA will be combined with the Matlab programming software and Finite Element Analysis (FEA) model in order to predict the damage location with respect to the prescribing boundaries and loadings conditions. The present works shows the application of the FEA of Abaqus / CAE software programming to build its graphical user interface (GUI) and Matlab software used to control its algorithms for its structural analysis in relation to the components. AKADEMIA BARU 2016-01-11 Article PeerReviewed Imran, Mohd. Salleh and Sarip, Shamsul and Muhtazaruddin, Mohd. Nabil and Hassan, Mohamad Zaki and Md. Daud, Mohd. Yusof and Abdul Aziz, Sa'ardin (2016) Structural health monitoring (SHM) on high stress loading of wing bracket. Journal of Advanced Research in Applied Mechanics, 27 (1). pp. 16-22. ISSN 2289-7895 http://www.myjurnal.my/public//article-view.php?id=103782
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
topic TL Motor vehicles. Aeronautics. Astronautics
spellingShingle TL Motor vehicles. Aeronautics. Astronautics
Imran, Mohd. Salleh
Sarip, Shamsul
Muhtazaruddin, Mohd. Nabil
Hassan, Mohamad Zaki
Md. Daud, Mohd. Yusof
Abdul Aziz, Sa'ardin
Structural health monitoring (SHM) on high stress loading of wing bracket
description This paper presents a Structural Health Monitoring (SHM) approach by addressing the modeling based on Cessna 310 wing bracket to collect its baseline data. SHM is a novel technology application in most engineering field including aircraft and aerospace field for defect detection including crack and other damage area. The main purpose of this project is to assess their structural integrity due to designated loading and boundary conditions using ABAQUS modeling technique application. These parts were selected as its structures are specifically complex and considered as ageing aircraft parts. The work can be also regarded as platform for CAD model database for ageing aircraft parts investigation upon their structural analyses and design preference. The works begins with a precise measurement using basic gauges and transfer to a 3-D solid modeling using CATIA V6. The optimization technique introduces in this work will be of a novel approach since the CATIA will be combined with the Matlab programming software and Finite Element Analysis (FEA) model in order to predict the damage location with respect to the prescribing boundaries and loadings conditions. The present works shows the application of the FEA of Abaqus / CAE software programming to build its graphical user interface (GUI) and Matlab software used to control its algorithms for its structural analysis in relation to the components.
format Article
author Imran, Mohd. Salleh
Sarip, Shamsul
Muhtazaruddin, Mohd. Nabil
Hassan, Mohamad Zaki
Md. Daud, Mohd. Yusof
Abdul Aziz, Sa'ardin
author_facet Imran, Mohd. Salleh
Sarip, Shamsul
Muhtazaruddin, Mohd. Nabil
Hassan, Mohamad Zaki
Md. Daud, Mohd. Yusof
Abdul Aziz, Sa'ardin
author_sort Imran, Mohd. Salleh
title Structural health monitoring (SHM) on high stress loading of wing bracket
title_short Structural health monitoring (SHM) on high stress loading of wing bracket
title_full Structural health monitoring (SHM) on high stress loading of wing bracket
title_fullStr Structural health monitoring (SHM) on high stress loading of wing bracket
title_full_unstemmed Structural health monitoring (SHM) on high stress loading of wing bracket
title_sort structural health monitoring (shm) on high stress loading of wing bracket
publisher AKADEMIA BARU
publishDate 2016
url http://eprints.utm.my/id/eprint/68433/
http://www.myjurnal.my/public//article-view.php?id=103782
_version_ 1643655946444996608
score 13.211869

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