Theoretically there is large thrust gain available by efficiently expanding exhaust gases at high aircraft speeds; methods of expanding exhaust by means of convergent-divergent nozzles; variable convergent-divergent nozzles, and ejector nozzles; typical installations; schematics and thrust increase curves; matching of air intakes and nozzles.


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    Title :

    Exhaust nozzles for supersonic aircraft


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Pearson, H. (author)

    Published in:

    Publication date :

    1958


    Size :

    5 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English