Conceptual design and optimal sizing of a small unmanned aerial vehicle with fuel cell and battery-powered hybrid propulsion system by meta-heuristic algorithms based on energy consumption-Reference-Cited by-同舟云学术

Conceptual design and optimal sizing of a small unmanned aerial vehicle with fuel cell and battery-powered hybrid propulsion system by meta-heuristic algorithms based on energy consumption

Published:2023-01-16 Issue:1 Volume:45 Page:140-159
ISSN:1556-7036
Container-title:Energy Sources, Part A: Recovery, Utilization, and Environmental Effects
language:en
Short-container-title:Energy Sources, Part A: Recovery, Utilization, and Environmental Effects

Author:

Çınar Hasan¹^ORCID,Tunçel Süleyman²^ORCID,Kandemir Ilyas³^ORCID,Gözel Tuba⁴^ORCID

Affiliation:

1. Faculty of Aeronautics and Astronautics, Iskenderun Technical University, Iskenderun, Turkey

2. Faculty of Engineering and Natural Sciences, Iskenderun Technical University, Iskenderun, Turkey

3. Aeronautical Engineering, Aerospace Faculty, Gebze Technical University, Gebze, Turkey

4. Electronics Engineering, Faculty of Engineering, Gebze Technical University, Gebze, Turkey

Publisher

Informa UK Limited

Subject

Energy Engineering and Power Technology,Fuel Technology,Nuclear Energy and Engineering,Renewable Energy, Sustainability and the Environment

Link

https://www.tandfonline.com/doi/pdf/10.1080/15567036.2023.2166166

Reference48 articles.

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2. Anderson, J. D. 1999. Aircraft Performance and Design. New York: McGraw-Hill Book Company.

3. Advanced Sizing Methodology for a Multi-Mode eVTOL UAV Powered by a Hydrogen Fuel Cell and Battery

4. Conceptual design analysis for a lightweight aircraft with a fuel cell hybrid propulsion system

5. Research on Energy Management of Hybrid Unmanned Aerial Vehicles to Improve Energy-Saving and Emission Reduction Performance

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