Study of flutter on a composite UAV wing

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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書目詳細資料
主要作者:	Zaki, Nurul Zubaidah
格式:	Thesis
語言:	English
出版:	2017
主題:	TJ Mechanical engineering and machinery
在線閱讀:	http://eprints.utm.my/id/eprint/78962/1/NurulZubaidahZakiMFKM2017.pdf
標簽:	添加標簽沒有標簽, 成為第一個標記此記錄!

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