Results of tests carried out at Nat Aeronautical Establishment, showed that best performance could be obtained with mixing tube length to width ratio of about 6; thrust augmentation ratio of 1.3 was obtained for secondary to primary area ratios greater than 19; further increase in thrust augmentation of 10% was achieved by diffusing mixing tube walls to total angle between 2 and 4°.


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    Titel :

    Experimental thrust augmentation of variable geometry, two-dimensional, central nozzle ejector


    Weitere Titelangaben:

    Can Aeronautics Space J


    Beteiligte:
    Drummond, A.M. (Autor:in) / Gould, D.G. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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    Drummond, A.M. / Gould, D.G. | Engineering Index Backfile | 1962



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