Syed Mohamed Ali, Jaffar and Jamaludin, Nur Faizlin and Roslan, Rosfarisya and Abdul Rahman, Mohammad (2011) Buckling of composite columns. In: Advances in Aircraft Structures. IIUM Press, Kuala Lumpur, pp. 107-116. ISBN 978-967-418-148-2
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Abstract
This chapter deals with the experimental procedure to evaluate the critical load, failure load and predict the mode of failure for the column speciments made of composite material. The type of section that is being considered is rectangular and both woven roving fiber and chopped strand mats fiber types of glass fibers have been examined.
Item Type: | Book Chapter |
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Uncontrolled Keywords: | Buckling, composites, columns, experimental, critical load |
Subjects: | T Technology > TA Engineering (General). Civil engineering (General) > TA630 Structural engineering (General) |
Kulliyyahs/Centres/Divisions/Institutes (Can select more than one option. Press CONTROL button): | Kulliyyah of Engineering > Department of Mechanical Engineering |
Depositing User: | Dr Mohamed Ali Jaffar Syed |
Date Deposited: | 16 Jul 2012 22:13 |
Last Modified: | 16 Jul 2012 22:13 |
URI: | http://irep.iium.edu.my/id/eprint/24898 |
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