Correction to

Analysis and design of hybrid electric regional turboprop aircraft (CEAS Aeronautical Journal, (2018), 9, 1, (15-25), 10.1007/s13272-017-0272-1)

Journal article (2019)

Authors

M. Voskuij Flight Performance and Propulsion - Aerospace Engineering
A. Rao Flight Performance and Propulsion - Aerospace Engineering
Research Group
Flight Performance and Propulsion (Aerospace Engineering) (TU Delft)
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Published Date

01-01-2019

Language

English

Reuse Rights

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Faculty

Aerospace Engineering

Department

Flow Physics and Technology

Research Group

Flight Performance and Propulsion

Abstract

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.

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