Crash Simulation Of A Composite Unmanned Aerial Vehicle Fuselage

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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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Bibliographic Details
Main Author:	Yidris, Noorfaizal
Format:	Thesis
Language:	English English
Published:	2007
Online Access:	http://psasir.upm.edu.my/id/eprint/5251/ http://psasir.upm.edu.my/id/eprint/5251/1/FK_2007_47.pdf

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