Necessity of designing tail pipe burners with low burner inlet velocity, low burner drag, and high diffuser efficiency in order to obtain both high thrust augmentation and to minimize loss in normal engine performance during nonburning operation is illustrated.


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    Title :

    Theoretical analysis of various thrust-augmentation cycles for turbojet engines


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1950


    Size :

    52 pages


    Remarks:

    Diagrams, Charts


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English