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LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow

The paper presents aeroelastic characteristics of a cantilevered composite wing, idealized as a composite flat plate laminate. The composite laminate was made from woven glass fibers with epoxy matrix. The elastic and dynamic properties of the laminate were determined experimentally for aeroelastic...

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Main Authors: Abang Abdul Majid, Dayang Laila, Basri, Shahnor
Format: Article
Language:English
Published: Springer 2008
Online Access:http://psasir.upm.edu.my/id/eprint/15425/1/LCO%20flutter%20of%20cantilevered%20woven%20glassepoxy%20laminate%20in%20subsonic%20flow.pdf
http://psasir.upm.edu.my/id/eprint/15425/
https://link.springer.com/article/10.1007/s10409-007-0117-y
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spelling my.upm.eprints.154252019-07-08T07:36:43Z http://psasir.upm.edu.my/id/eprint/15425/ LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow Abang Abdul Majid, Dayang Laila Basri, Shahnor The paper presents aeroelastic characteristics of a cantilevered composite wing, idealized as a composite flat plate laminate. The composite laminate was made from woven glass fibers with epoxy matrix. The elastic and dynamic properties of the laminate were determined experimentally for aeroelastic calculations. Aeroelastic wind tunnel testing of the laminate was performed and the result showed that flutter, a dynamic instability occurred. The cantilevered laminate also displayed limit cycle amplitude, post-flutter oscillation. The experimental flutter velocity and frequency were verified by our computational analysis. Springer 2008 Article PeerReviewed text en http://psasir.upm.edu.my/id/eprint/15425/1/LCO%20flutter%20of%20cantilevered%20woven%20glassepoxy%20laminate%20in%20subsonic%20flow.pdf Abang Abdul Majid, Dayang Laila and Basri, Shahnor (2008) LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow. Acta Mechanica Sinica, 24 (1). pp. 107-110. ISSN 0567-7718; ESSN: 1614-3116 https://link.springer.com/article/10.1007/s10409-007-0117-y 10.1007/s10409-007-0117-y
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
description The paper presents aeroelastic characteristics of a cantilevered composite wing, idealized as a composite flat plate laminate. The composite laminate was made from woven glass fibers with epoxy matrix. The elastic and dynamic properties of the laminate were determined experimentally for aeroelastic calculations. Aeroelastic wind tunnel testing of the laminate was performed and the result showed that flutter, a dynamic instability occurred. The cantilevered laminate also displayed limit cycle amplitude, post-flutter oscillation. The experimental flutter velocity and frequency were verified by our computational analysis.
format Article
author Abang Abdul Majid, Dayang Laila
Basri, Shahnor
spellingShingle Abang Abdul Majid, Dayang Laila
Basri, Shahnor
LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow
author_facet Abang Abdul Majid, Dayang Laila
Basri, Shahnor
author_sort Abang Abdul Majid, Dayang Laila
title LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow
title_short LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow
title_full LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow
title_fullStr LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow
title_full_unstemmed LCO flutter of cantilevered woven glass/epoxy laminate in subsonic flow
title_sort lco flutter of cantilevered woven glass/epoxy laminate in subsonic flow
publisher Springer
publishDate 2008
url http://psasir.upm.edu.my/id/eprint/15425/1/LCO%20flutter%20of%20cantilevered%20woven%20glassepoxy%20laminate%20in%20subsonic%20flow.pdf
http://psasir.upm.edu.my/id/eprint/15425/
https://link.springer.com/article/10.1007/s10409-007-0117-y
_version_ 1643825930756423680
score 13.211869

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