A method for an efficiency and weight-optimised preliminary design of a hydrogen-powered fuel cell-based hybrid-electric propulsion system for aviation purposes.

Autor: Akkaya, Mücahit, Neumann, Nicolai, Peitsch, Dieter
Zdroj: CEAS Aeronautical Journal; Apr2024, Vol. 15 Issue 2, p175-189, 15p
Databáze: Complementary Index