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)

Mark Voskuijl; Joris van Bogaert; Arvind G. Rao

doi:10.1007/s13272-019-00428-8

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)

Mark Voskuijl^*, Joris van Bogaert, Arvind G. Rao

^*Corresponding author for this work

Flight Performance and Propulsion

Research output: Contribution to journal › Comment/Letter to the editor › Scientific

1 Citation (Scopus)

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.

Original language	English
Pages (from-to)	303
Number of pages	1
Journal	CEAS Aeronautical Journal
Volume	11
Issue number	1
DOIs	https://doi.org/10.1007/s13272-019-00428-8
Publication status	Published - 1 Jan 2019

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title = "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)",

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.",

author = "Mark Voskuijl and {van Bogaert}, Joris and Rao, {Arvind G.}",

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T2 - Analysis and design of hybrid electric regional turboprop aircraft (CEAS Aeronautical Journal, (2018), 9, 1, (15-25), 10.1007/s13272-017-0272-1)

AU - Voskuijl, Mark

AU - van Bogaert, Joris

AU - Rao, Arvind G.

PY - 2019/1/1

Y1 - 2019/1/1

N2 - 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.

AB - 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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U2 - 10.1007/s13272-019-00428-8

DO - 10.1007/s13272-019-00428-8

M3 - Comment/Letter to the editor

AN - SCOPUS:85074034706

SN - 1869-5582

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SP - 303

JO - CEAS Aeronautical Journal

JF - CEAS Aeronautical Journal

IS - 1

ER -

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)

Abstract

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