UPM Institutional Repository

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


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


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.

Download File

Text (Abstract)
LCO flutter of cantilevered woven glassepoxy laminate in subsonic flow.pdf

Download (35kB) | Preview

Additional Metadata

Item Type: Article
Divisions: Faculty of Engineering
DOI Number: https://doi.org/10.1007/s10409-007-0117-y
Publisher: Springer
Keywords: Limit cycle oscillation; Flutter; Laminate
Depositing User: Nabilah Mustapa
Date Deposited: 08 Jul 2019 07:36
Last Modified: 08 Jul 2019 07:36
Altmetrics: http://www.altmetric.com/details.php?domain=psasir.upm.edu.my&doi=10.1007/s10409-007-0117-y
URI: http://psasir.upm.edu.my/id/eprint/15425
Statistic Details: View Download Statistic

Actions (login required)

View Item View Item