Study of flutter on a composite UAV wing
A study of flutter of the VAV composite wing has been done by considering the aeroelasticity phenomenon which involves the dynamic instability of a structure which able to lead a catastrophic failure. To prevent any failure, various design effects and materials parameters of the wing structure for a...
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| 主要作者: | |
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| 格式: | Thesis |
| 語言: | English |
| 出版: |
2017
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| 主題: | |
| 在線閱讀: | http://eprints.utm.my/id/eprint/78962/1/NurulZubaidahZakiMFKM2017.pdf |
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