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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מידע ביבליוגרפי

Principais autores:	M. Rostami, A.H. Farajollahi, M. Marefati, R. Fili, F. Bagherpor
פורמט:	Artigo
שפה:	Inglês
יצא לאור:	Shahrood University of Technology 2022-07-01
סדרה:	Renewable Energy Research and Applications
נושאים:	uav sofc fuel cell turbine-less jet engine supersonic multi-objective optimization
גישה מקוונת:	https://rera.shahroodut.ac.ir/article_2349_95b0926b7b8e68eda8c890f0087dc0a1.pdf
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