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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Egile Nagusiak:	M. Rostami, A.H. Farajollahi, M. Marefati, R. Fili, F. Bagherpor
Formatua:	Artigo
Hizkuntza:	Inglês
Argitaratua:	Shahrood University of Technology 2022-07-01
Saila:	Renewable Energy Research and Applications
Gaiak:	uav sofc fuel cell turbine-less jet engine supersonic multi-objective optimization
Sarrera elektronikoa:	https://rera.shahroodut.ac.ir/article_2349_95b0926b7b8e68eda8c890f0087dc0a1.pdf
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