Structural design improvement of unmanned aerial vehicle wing

Structural design improvement of unmanned aerial vehicle wing

Almost all engineering systems experience strength versus weight conflict of some description. In the case of airplane wing, there are two primary requirements which must be considered during the structural design process: high strength and stiffness, and lower weight. Due to the restricted nature o...

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书目详细资料
主要作者:	Kanesan, Gunasegaran
格式:	Thesis
语言:	English
出版:	2014
主题:	TJ Mechanical engineering and machinery
在线阅读:	http://eprints.utm.my/id/eprint/53465/25/GunasegaranKanesanMFKM2014.pdf
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