A comparative Analysis and Optimization of two Supersonic Hybrid Solid Oxide Fuel Cell and Turbine-less Jet Engine Propulsion Systems for Unmanned Aerial Vehicles
The propulsion system of an Unmanned Aerial Vehicle (UAV) plays an essential role in its performance, stability and flight endurance. In this study, two types of propulsion systems for UAV (differentiated based on fuel type) are studied to determine their characteristics and advantages. These propos...
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| Principais autores: | , , , , |
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| Formato: | Artigo |
| Idioma: | Inglês |
| Publicado: |
Shahrood University of Technology
2022-07-01
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| Series: | Renewable Energy Research and Applications |
| Assuntos: | |
| Acceso en liña: | https://rera.shahroodut.ac.ir/article_2349_95b0926b7b8e68eda8c890f0087dc0a1.pdf |
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