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)
Author(s)
Mark Voskuijl (TU Delft - Flight Performance and Propulsion)
Joris van Bogaert (Student TU Delft)
Arvind G. Rao (TU Delft - Flight Performance and Propulsion)
Research Group
Flight Performance and Propulsion
DOI related publication
https://doi.org/10.1007/s13272-019-00428-8
To reference this document use:
https://resolver.tudelft.nl/uuid:d3bf5e23-2c5d-4373-8b1e-101aba303577
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Publication Year
2019
Language
English
Research Group
Flight Performance and Propulsion
Issue number
1
Volume number
11
Pages (from-to)
303
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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