Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach
Shape memory alloy was firstly used commercially as a hydraulic coupling in the Grumman F14A in 1971. It is today used among others to improve structural behaviours such as buckling of composite plates in the aerospace vehicles. In this paper, finite element model and its source code for thermal pos...
| Main Authors: | , , , , |
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| Format: | Article |
| Language: | English |
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Trans Tech Publications
2011
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| Online Access: | http://psasir.upm.edu.my/id/eprint/23371/ http://psasir.upm.edu.my/id/eprint/23371/1/Thermal%20post-buckling%20improvements%20of%20laminated%20composite%20plates%20using%20the%20active%20strain%20energy%20tuning%20approach.pdf |
| _version_ | 1848844739519971328 |
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| author | A. Rasid, Zainudin Zahari, Rizal Ayob, Amran Abang Abdul Majid, Dayang Laila Mohd Rafie, Azmin Shakrine |
| author_facet | A. Rasid, Zainudin Zahari, Rizal Ayob, Amran Abang Abdul Majid, Dayang Laila Mohd Rafie, Azmin Shakrine |
| author_sort | A. Rasid, Zainudin |
| building | UPM Institutional Repository |
| collection | Online Access |
| description | Shape memory alloy was firstly used commercially as a hydraulic coupling in the Grumman F14A in 1971. It is today used among others to improve structural behaviours such as buckling of composite plates in the aerospace vehicles. In this paper, finite element model and its source code for thermal post-buckling of shape memory alloy laminated composite plates is presented. The shape memory alloy wires induced stress that improved the strain energy, stiffness and thus the buckling behaviour of the composite plates. The finite element formulation catered the combined properties of the composite and shape memory alloys, the addition of the recovery stress and the temperature dependent properties of the shape memory alloys and the composite matrix. This study showed that by embedding shape memory alloy within layers of composite plates, post-buckling behaviours of composite plates can be improved substantially. |
| first_indexed | 2025-11-15T08:35:43Z |
| format | Article |
| id | upm-23371 |
| institution | Universiti Putra Malaysia |
| institution_category | Local University |
| language | English |
| last_indexed | 2025-11-15T08:35:43Z |
| publishDate | 2011 |
| publisher | Trans Tech Publications |
| recordtype | eprints |
| repository_type | Digital Repository |
| spelling | upm-233712015-12-04T07:07:45Z http://psasir.upm.edu.my/id/eprint/23371/ Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach A. Rasid, Zainudin Zahari, Rizal Ayob, Amran Abang Abdul Majid, Dayang Laila Mohd Rafie, Azmin Shakrine Shape memory alloy was firstly used commercially as a hydraulic coupling in the Grumman F14A in 1971. It is today used among others to improve structural behaviours such as buckling of composite plates in the aerospace vehicles. In this paper, finite element model and its source code for thermal post-buckling of shape memory alloy laminated composite plates is presented. The shape memory alloy wires induced stress that improved the strain energy, stiffness and thus the buckling behaviour of the composite plates. The finite element formulation catered the combined properties of the composite and shape memory alloys, the addition of the recovery stress and the temperature dependent properties of the shape memory alloys and the composite matrix. This study showed that by embedding shape memory alloy within layers of composite plates, post-buckling behaviours of composite plates can be improved substantially. Trans Tech Publications 2011 Article PeerReviewed application/pdf en http://psasir.upm.edu.my/id/eprint/23371/1/Thermal%20post-buckling%20improvements%20of%20laminated%20composite%20plates%20using%20the%20active%20strain%20energy%20tuning%20approach.pdf A. Rasid, Zainudin and Zahari, Rizal and Ayob, Amran and Abang Abdul Majid, Dayang Laila and Mohd Rafie, Azmin Shakrine (2011) Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach. Advanced Materials Research, 311-313. pp. 2235-2238. ISSN 1022-6680; ESSN: 1662-8985 http://www.scientific.net/AMR.311-313.2235 10.4028/www.scientific.net/AMR.311-313.2235 |
| spellingShingle | A. Rasid, Zainudin Zahari, Rizal Ayob, Amran Abang Abdul Majid, Dayang Laila Mohd Rafie, Azmin Shakrine Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach |
| title | Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach |
| title_full | Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach |
| title_fullStr | Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach |
| title_full_unstemmed | Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach |
| title_short | Thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach |
| title_sort | thermal post-buckling improvements of laminated composite plates using the active strain energy tuning approach |
| url | http://psasir.upm.edu.my/id/eprint/23371/ http://psasir.upm.edu.my/id/eprint/23371/ http://psasir.upm.edu.my/id/eprint/23371/ http://psasir.upm.edu.my/id/eprint/23371/1/Thermal%20post-buckling%20improvements%20of%20laminated%20composite%20plates%20using%20the%20active%20strain%20energy%20tuning%20approach.pdf |