Optimization Of Composite Hinges For Aircraft Spoiler Using Finite Element Method
Current hinge brackets for A320 aircraft are made from metallic materials. The change of material from metallic to composite can reduce the structure weight. The classical method of analysis such as hand calculation and actual testing are not recommended for the new composite hinge design because it...
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| Format: | Thesis |
| Language: | English English |
| Published: |
2019
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| Subjects: | |
| Online Access: | http://eprints.utem.edu.my/id/eprint/24508/1/Optimization%20Of%20Composite%20Hinges%20For%20Aircraft%20Spoiler%20Using%20Finite%20Element%20Method.pdf http://eprints.utem.edu.my/id/eprint/24508/2/Optimization%20Of%20Composite%20Hinges%20For%20Aircraft%20Spoiler%20Using%20Finite%20Element%20Method.pdf |
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http://eprints.utem.edu.my/id/eprint/24508/1/Optimization%20Of%20Composite%20Hinges%20For%20Aircraft%20Spoiler%20Using%20Finite%20Element%20Method.pdfhttp://eprints.utem.edu.my/id/eprint/24508/2/Optimization%20Of%20Composite%20Hinges%20For%20Aircraft%20Spoiler%20Using%20Finite%20Element%20Method.pdf