期刊论文详细信息
American journal of engineering and applied sciences | |
Low Reynolds Number Wing Design for Unmanned Aerial Vehicle: A Case Study | |
article | |
Mohammed El-Adawy1  Alhassan H. Farid1  Mohamed Ahmed Hassan1  Mahmoud Abady1  Donia Medhat1  Habiba Abdullatif1  Omar Hassan1  Salaheldin Mohamed Thabet1  | |
[1]Department of Mechanical Engineering, Faculty of Engineering, Alexandria University | |
关键词: UAV; Wing Design; Low Reynolds Number; | |
DOI : 10.3844/ajeassp.2022.264.273 | |
学科分类:工程和技术(综合) | |
来源: Science Publications | |
【 摘 要 】
With the widespread utilization of Unmanned Aerial Vehicles (UAVs) in many fields, it is essential to identify the parameters governing their design process. By taking the wing as a showcase, this study intends to guide through the design process of the wing, elaborate on some important definitions, and show how different parts of an aircraft affect each other. The current case study is limited to low Reynolds number (200,000: 500,000) wing design for unmanned aerial vehicle. The final wing was designed to be rectangular, a high wing with a span of 2 m, a chord of 0.4 m, and a corresponding aspect ratio of 5 with a total take-off weight of 10 kg. While the cruising speed and stall speeds were 14 and 11 m/s respectively.【 授权许可】
CC BY
【 预 览 】
Files | Size | Format | View |
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RO202307060002292ZK.pdf | 721KB | download |