TY - JOUR AU - El-Adawy, Mohammed AU - H. Farid, Alhassan AU - Hassan, Mohamed Ahmed AU - Abady, Mahmoud AU - Medhat, Donia AU - Abdullatif, Habiba AU - Hassan, Omar AU - Thabet, Salaheldin Mohamed PY - 2022 TI - Low Reynolds Number Wing Design for Unmanned Aerial Vehicle: A Case Study JF - American Journal of Engineering and Applied Sciences VL - 15 IS - 4 DO - 10.3844/ajeassp.2022.264.273 UR - https://thescipub.com/abstract/ajeassp.2022.264.273 AB - 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.