Analysis of composite box beam with piezoelectric actuators using ANSYS
In this work the potential of piezoelectric actuators to induce twist on a composite helicopter rotor blade has been investigated using ANSYS. An analogical thin-walled box beam has been modeled to investigate the effects of different ply orientations, boundary conditions and applied loads on displa...
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iium-331412013-12-26T01:08:03Z http://irep.iium.edu.my/33141/ Analysis of composite box beam with piezoelectric actuators using ANSYS Syed Mohamed Ali, Jaffar Shaik Dawood, Mohd. Sultan Ibrahim Syed Muhammad, Kashif Tariq, M. TL500 Aeronautics In this work the potential of piezoelectric actuators to induce twist on a composite helicopter rotor blade has been investigated using ANSYS. An analogical thin-walled box beam has been modeled to investigate the effects of different ply orientations, boundary conditions and applied loads on displacement and twist of the box beam. Results obtained confirm piezoelectric actuators can be effectively used for the said purpose. Significant influences of boundary conditions and ply orientations were observed on the deformation and twist output. Although the studies were carried out on a simple box beam model, the output from this work could serve as a useful reference for future work. 2013 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/33141/1/Paper_30168_-_Camera_ready.pdf Syed Mohamed Ali, Jaffar and Shaik Dawood, Mohd. Sultan Ibrahim and Syed Muhammad, Kashif and Tariq, M. (2013) Analysis of composite box beam with piezoelectric actuators using ANSYS. In: International Conference on Mechanical, Automotive and Aerospace Engineering (ICMAAE' 13), 2nd-4th Jul. 2013, Kuala Lumpur, Malaysia. |
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International Islamic University Malaysia |
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English |
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TL500 Aeronautics |
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TL500 Aeronautics Syed Mohamed Ali, Jaffar Shaik Dawood, Mohd. Sultan Ibrahim Syed Muhammad, Kashif Tariq, M. Analysis of composite box beam with piezoelectric actuators using ANSYS |
description |
In this work the potential of piezoelectric actuators to induce twist on a composite helicopter rotor blade has been investigated using ANSYS. An analogical thin-walled box beam has been modeled to investigate the effects of different ply orientations, boundary conditions and applied loads on displacement and twist of the box beam. Results obtained confirm piezoelectric actuators can be effectively used for the said purpose. Significant influences of boundary conditions and ply orientations were observed on the deformation and twist output. Although the studies were carried out on a simple box beam model, the output from this work could serve as a useful reference for future work. |
format |
Conference or Workshop Item |
author |
Syed Mohamed Ali, Jaffar Shaik Dawood, Mohd. Sultan Ibrahim Syed Muhammad, Kashif Tariq, M. |
author_facet |
Syed Mohamed Ali, Jaffar Shaik Dawood, Mohd. Sultan Ibrahim Syed Muhammad, Kashif Tariq, M. |
author_sort |
Syed Mohamed Ali, Jaffar |
title |
Analysis of composite box beam with piezoelectric actuators using ANSYS |
title_short |
Analysis of composite box beam with piezoelectric actuators using ANSYS |
title_full |
Analysis of composite box beam with piezoelectric actuators using ANSYS |
title_fullStr |
Analysis of composite box beam with piezoelectric actuators using ANSYS |
title_full_unstemmed |
Analysis of composite box beam with piezoelectric actuators using ANSYS |
title_sort |
analysis of composite box beam with piezoelectric actuators using ansys |
publishDate |
2013 |
url |
http://irep.iium.edu.my/33141/ http://irep.iium.edu.my/33141/1/Paper_30168_-_Camera_ready.pdf |
first_indexed |
2023-09-18T20:47:53Z |
last_indexed |
2023-09-18T20:47:53Z |
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1777409797131337728 |