Modeling And Analysis Of Composite Hinge For Aircraft Spoiler Using Finite Element Analysis
This thesis is concerned with the modeling and analysis of a composite hinge bracket for Airbus A320 aircraft using Finite Element Method. The increasing demand of composite materials in aircraft structural design is due to the high strength and stiffness to weight ratio of the composite materials....
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| Format: | Thesis |
| Language: | English English |
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2014
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| Online Access: | http://eprints.utem.edu.my/id/eprint/15010/ https://plh.utem.edu.my/cgi-bin/koha/opac-detail.pl?biblionumber=92071 |
| Abstract | Abstract here |