Calibration test results and characteristics test data of both static force tests and autorotation tests; velocity, at model location, is uniform within 0.2% and air flow direction is parallel to axis of jet within 0.3%.


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    Title :

    7 by 10 foot wind tunnel of National Advisory Committee for Aeronautics


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1931


    Size :

    9 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :