The primary objective of a liquid fuel injection system is to provide the combustion chamber with the proper amount of fuel and with a spatial pattern that will result in efficient combustion over the entire flight path of the ramjet. In [1], empirical methods for designing fuel injectors were defined. In this work, the approach of Wu [2] to calculate the breakup time of the jet, the correlation of Lefevbre [3] for the average diameter of the droplets of fuel, the study of Turns [4] to calculate the time of vaporization of the droplet and the data processed by Kundu, Colket and Fuller [5–7] for the delay have been selected to provide guidelines to injector design.


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    Titel :

    Injector Design Guidelines


    Weitere Titelangaben:

    SpringerBriefs in Applied Sciences


    Beteiligte:


    Erscheinungsdatum :

    2021-01-30


    Format / Umfang :

    11 pages





    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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