Problem of pure jet aircraft take-off distance is indicated, and basic reasons for excess thrust deficiency as compared to propeller aircraft shown; afterburner concept discussed; thrust augmentations of 45% low speed and over 100% high speed shown to be feasible; method for analyzing afterburners. (See also - discussion n 9 Sept p 521)


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    Title :

    Afterburners for turbojet engines


    Additional title:

    J Aeronautical Sciences


    Contributors:


    Publication date :

    1948


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English





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