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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    Title :

    Injector Design Guidelines


    Additional title:

    SpringerBriefs in Applied Sciences


    Contributors:


    Publication date :

    2021-01-30


    Size :

    11 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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