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: Zaki, Nurul Zubaidah
格式: Thesis
语言:English
出版: 2017
主题:
在线阅读:http://eprints.utm.my/id/eprint/78962/1/NurulZubaidahZakiMFKM2017.pdf
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