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Crush simulation of woven c-glass/epoxy unmanned ariel vehicle fuselage section

A quasi-static crush analysis of an unmanned aerial vehicle (UAV) fuselage section made of woven c-glass/epoxy has been conducted using the finite element simulation via ABAQUS. The main material and strength properties of the c-glass/epoxy (200 g/m2) which were needed in the ABAQUS analyses were ob...

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Bibliographic Details
Main Authors: Yidris, Noorfaizal, Zahari, Rizal, Abang Abdul Majid, Dayang Laila, Mustapha, Faizal, Hameed Sultan, Mohamed Thariq, Mohd Rafie, Azmin Shakrine
Format: Article
Language:English
Published: Department of Mechanical Engineering, University of Malaya 2010
Online Access:http://psasir.upm.edu.my/id/eprint/13833/1/Crush%20simulation%20of%20woven%20c-glassepoxy%20unmanned%20ariel%20vehicle%20fuselage%20section.pdf
http://psasir.upm.edu.my/id/eprint/13833/
http://ejum.fsktm.um.edu.my/ArticleInformation.aspx?ArticleID=1002
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http://psasir.upm.edu.my/id/eprint/13833/1/Crush%20simulation%20of%20woven%20c-glassepoxy%20unmanned%20ariel%20vehicle%20fuselage%20section.pdf
http://psasir.upm.edu.my/id/eprint/13833/
http://ejum.fsktm.um.edu.my/ArticleInformation.aspx?ArticleID=1002

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