Design, analysis and weight optimization of a UAV wing
This thesis is a study of the design and optimization of a small wing, which will satisfy specific requirements for the mission of an unmanned aerial vehicle. In the design process, the determination of the initial individual values of the construction weight of the air vehicle was carried out by an...
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| Language: | English |
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2022
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| Online Access: | https://hdl.handle.net/10889/23412 |
