Wind tunnel tests made on three tubes with flow regulated by suction at trailing edge; it was possible to vary mass flow through tube over large range; it is indicated that thrust of shrouded propeller can be increased at low forward speeds by suction at trailing edge of shroud. English translation from (ZWB) Deutsche Luftfahrtforschung -- Forschungsbericht n 1945 May 19 1944.


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    Title :

    Venturi tube with varying mass flow


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Contributors:


    Publication date :

    1948


    Size :

    31 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    Venturi tube with varying mass flow

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