Successful tests carried out on Turbomeca jet unit with variable augmentation by ducted fan, developed in France; it embodies variable circulation system evolved by M.SZYDLOWSKI in which ratio of augmentation is controllable to establish optimum propulsive efficiency over range of aircraft speeds; it incorporates " centrifugal injection" system in which fuel, supplied along main shaft, is atomized and projected into annular combustion chamber through radial holes in thrower flange.


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    Titel :

    Aspin I.


    Weitere Titelangaben:

    Flight


    Erschienen in:

    Flight ; 59 , n 2193


    Erscheinungsdatum :

    1951


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch




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