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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| 格式: | Thesis |
| 语言: | English |
| 出版: |
2014
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| 主题: | |
| 在线阅读: | http://eprints.utm.my/id/eprint/53465/25/GunasegaranKanesanMFKM2014.pdf |
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