Design of a hybrid turbo-electric propulsion (HTEP) with fuel cells for a regional aircraft with 80 seats. Demonstration and verification of some solutions for HTEP. - Login required - Scipedia

9th European Congress on Computational Methods in Applied Sciences and Engineering

M. Kirichkov, S. Dmytriyev, O. Yelanskiy, I. Kravchenko

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Published on 29/10/24
Submitted on 29/10/24

DOI: 10.23967/eccomas.2024.251
Licence: CC BY-NC-SA license

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Keywords

Regional aircraft • Hybrid turboelectric propulsion • Hybridization level • Hydrogen

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