Crash Simulation Of A Composite Unmanned Aerial Vehicle Fuselage

In this research the results of experimental works and numerical simulation works pertaining to the crash behavior and crashworthiness characteristic of the upper part of the composite unmanned aerial vehicle (UAV) fuselage sections that were subjected to quasi-static transverse compressive loading...

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主要作者: Yidris, Noorfaizal
格式: Thesis
语言:English
English
出版: 2007
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在线阅读:http://psasir.upm.edu.my/id/eprint/5251/1/FK_2007_47.pdf
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