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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    Title :

    Correction to: Analysis and design of hybrid electric regional turboprop aircraft


    Additional title:

    CEAS Aeronaut J


    Contributors:

    Published in:

    Publication date :

    2020-01-01


    Size :

    1 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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