Calculated and experimentally determined explosion pressure ratios obtained in combustion chamber presented over range of fuel air ratios; effects investigated; values of jet thrust and thrust specific fuel consumption obtained from this combustion chamber.


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    Title :

    Analytical and experimental performance of explosion-cycle combustion chamber for jet-propulsion engine


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1948


    Size :

    59 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English