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Abdul Redha, Haura, Reja, Ahmed, Shandookh, Ahmed. (1403). An Auxiliary Power System Based on Solar Photovoltaic for Enhanced Unmanned Aerial Vehicle Remote-Controlled Aircraft Endurance. , 10(1), 2223-2233. doi: 10.22059/jser.2025.398475.1596
Haura Haider Abdul Redha; Ahmed Hameed Reja; Ahmed Adnan Shandookh. "An Auxiliary Power System Based on Solar Photovoltaic for Enhanced Unmanned Aerial Vehicle Remote-Controlled Aircraft Endurance". , 10, 1, 1403, 2223-2233. doi: 10.22059/jser.2025.398475.1596
Abdul Redha, Haura, Reja, Ahmed, Shandookh, Ahmed. (1403). 'An Auxiliary Power System Based on Solar Photovoltaic for Enhanced Unmanned Aerial Vehicle Remote-Controlled Aircraft Endurance', , 10(1), pp. 2223-2233. doi: 10.22059/jser.2025.398475.1596
Abdul Redha, Haura, Reja, Ahmed, Shandookh, Ahmed. An Auxiliary Power System Based on Solar Photovoltaic for Enhanced Unmanned Aerial Vehicle Remote-Controlled Aircraft Endurance. , 1403; 10(1): 2223-2233. doi: 10.22059/jser.2025.398475.1596

An Auxiliary Power System Based on Solar Photovoltaic for Enhanced Unmanned Aerial Vehicle Remote-Controlled Aircraft Endurance

Journal of Solar Energy Research
دوره 10، شماره 1، فروردین 2025، صفحه 2223-2233    اصل مقاله (866.43 K)
نوع مقاله: Research Article
شناسه دیجیتال (DOI): 10.22059/jser.2025.398475.1596
نویسندگان
Haura Haider Abdul Redha* 1؛ Ahmed Hameed Reja2؛ Ahmed Adnan Shandookh3
1College of Electromechanical Engineering ,University of Technology-Iraq, Al-Wehda neighborhood ,Baghdad, Iraq
2College of Electromechanical Engineering, University of Technology-Iraq, Al-Wehda neighborhood, Baghdad, Iraq
3College of Mechanical Engineering, University of Technology-Iraq, Al-Wehda neighborhood, Baghdad, Iraq
چکیده
This research outlines the design, simulation, and structural evaluation of a solar-assisted power augmentation system integrated into an unmanned aerial vehicle (UAV) made of expanded polypropylene (EPP) foam. The system consists of two 1.5 W rigid monocrystalline solar panels mounted on the wings and an 18 W flexible panel mounted below the fuselage, which increased the UAV’s weight from 170 g to 840 g. Aerodynamic performance was assessed using computational fluid dynamics (CFD) simulations in ANSYS Fluent over a sweep of angles of attack (–6° to 12°) at speeds of 10 m/s and 30 m/s. The results showed lift augmentation of over 300% with significant drag reduction. Structural simulations in ANSYS Mechanical using pressure loads from CFD results confirmed that the maximum principal stress and von Mises strain were kept within 70% of the material limits of the EPP foam. The most effective operating range was found to be between 3° and 9° AoA for low-speed flight and between 0° and 6° AoA for high-speed flight. This study confirms the feasibility of integrating monocrystalline solar modules into lightweight UAVs as a viable method of drastically extending flight endurance without sacrificing aerodynamic or structural integrity.
کلیدواژه‌ها
UAV؛ Solar‐Power Augmentation؛ CFD؛ ANSYS Fluent؛ Static Structural Analysis؛ EPP‐Foam
مراجع
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آمار
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