There is an error in Equation 21 of the original article. The weight of the battery is a function of the energy stored at the start and will not vary during flight whereas the fuel weight will vary as a function of the energy level. Hence, the correct equation is.
Correction to: Analysis and design of hybrid electric regional turboprop aircraft
CEAS Aeronautical Journal ; 11 , 1 ; 303-303
2019
Aufsatz (Zeitschrift)
Englisch
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