Thermal buckling and post-buckling improvements of laminated composite plates using finite element method
Thermal buckling and thermal post-buckling behaviours of laminated composite plates are improved by embedding shape memory alloy wires within laminates of composite plates. The procedure is to use the recovery stress that is induced when the reverse transformation of the shape memory alloy from mart...
Saved in:
Main Authors: | , , , , , |
---|---|
Format: | Book Section |
Published: |
Scientific.net
2011
|
Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/30100/ http://dx.doi.org/10.4028/www.scientific.net/KEM.471-472.536 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
id |
my.utm.30100 |
---|---|
record_format |
eprints |
spelling |
my.utm.301002017-02-04T06:55:08Z http://eprints.utm.my/id/eprint/30100/ Thermal buckling and post-buckling improvements of laminated composite plates using finite element method A. Rasid, Zainudin Ayob, Amran Zahari, Rizal Mustapha, F. Majid, D. L. Varatharajoo, Renuganth TJ Mechanical engineering and machinery Thermal buckling and thermal post-buckling behaviours of laminated composite plates are improved by embedding shape memory alloy wires within laminates of composite plates. The procedure is to use the recovery stress that is induced when the reverse transformation of the shape memory alloy from martensite to austenite phases is constrained. For aerospace applications where the source of the shape memory alloy heating is the high temperature environment itself, a study is conducted to see the effect of shape memory alloy in improving the thermal buckling and postbuckling of composite plates. Due to the temperature dependent nature of the composite matrix and the shape memory alloy, the finite element formulation developed here is in the incremental form. Solving this non-linear model using the developed in-house source code, critical loads are determined and the post-buckling paths of the shape memory alloy composite plates are traced. This study shows that by embedding the shape memory alloy within composite plates, the thermal buckling and post-buckling behaviours of composite plates can be improved substantially. Scientific.net 2011 Book Section PeerReviewed A. Rasid, Zainudin and Ayob, Amran and Zahari, Rizal and Mustapha, F. and Majid, D. L. and Varatharajoo, Renuganth (2011) Thermal buckling and post-buckling improvements of laminated composite plates using finite element method. In: Key Engineering Materials. Scientific.net, Kuala Lumpur, pp. 536-541. ISBN 978-303785059-6 http://dx.doi.org/10.4028/www.scientific.net/KEM.471-472.536 10.4028/www.scientific.net/KEM.471-472.536 |
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 |
TJ Mechanical engineering and machinery |
spellingShingle |
TJ Mechanical engineering and machinery A. Rasid, Zainudin Ayob, Amran Zahari, Rizal Mustapha, F. Majid, D. L. Varatharajoo, Renuganth Thermal buckling and post-buckling improvements of laminated composite plates using finite element method |
description |
Thermal buckling and thermal post-buckling behaviours of laminated composite plates are improved by embedding shape memory alloy wires within laminates of composite plates. The procedure is to use the recovery stress that is induced when the reverse transformation of the shape memory alloy from martensite to austenite phases is constrained. For aerospace applications where the source of the shape memory alloy heating is the high temperature environment itself, a study is conducted to see the effect of shape memory alloy in improving the thermal buckling and postbuckling of composite plates. Due to the temperature dependent nature of the composite matrix and the shape memory alloy, the finite element formulation developed here is in the incremental form. Solving this non-linear model using the developed in-house source code, critical loads are determined and the post-buckling paths of the shape memory alloy composite plates are traced. This study shows that by embedding the shape memory alloy within composite plates, the thermal buckling and post-buckling behaviours of composite plates can be improved substantially. |
format |
Book Section |
author |
A. Rasid, Zainudin Ayob, Amran Zahari, Rizal Mustapha, F. Majid, D. L. Varatharajoo, Renuganth |
author_facet |
A. Rasid, Zainudin Ayob, Amran Zahari, Rizal Mustapha, F. Majid, D. L. Varatharajoo, Renuganth |
author_sort |
A. Rasid, Zainudin |
title |
Thermal buckling and post-buckling improvements of laminated composite plates using finite element method |
title_short |
Thermal buckling and post-buckling improvements of laminated composite plates using finite element method |
title_full |
Thermal buckling and post-buckling improvements of laminated composite plates using finite element method |
title_fullStr |
Thermal buckling and post-buckling improvements of laminated composite plates using finite element method |
title_full_unstemmed |
Thermal buckling and post-buckling improvements of laminated composite plates using finite element method |
title_sort |
thermal buckling and post-buckling improvements of laminated composite plates using finite element method |
publisher |
Scientific.net |
publishDate |
2011 |
url |
http://eprints.utm.my/id/eprint/30100/ http://dx.doi.org/10.4028/www.scientific.net/KEM.471-472.536 |
_version_ |
1643648455107674112 |
score |
13.211869 |