Finite element modelling of vibration characteristics of aircraft wing structure
This project provides a theoretical review and investigation of the vibration characteristics of an aircraft wing structure using the Finite Element Method. The vibration characteristics would include its natural frequencies and the different mode shapes of vibrations. The modal analysis was carri...
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| 格式: | Final Year Project |
| 語言: | English |
| 出版: |
2009
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| 主題: | |
| 在線閱讀: | http://hdl.handle.net/10356/16719 |
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| 機構: | Nanyang Technological University |
| 語言: | English |