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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| 格式: | Thesis |
| 語言: | English English |
| 出版: |
2007
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| 主題: | |
| 在線閱讀: | http://psasir.upm.edu.my/id/eprint/5251/1/FK_2007_47.pdf |
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