Propellers were mounted in front of liquid cooled engine nacelle and were tested at 15 different blade angles in range from -7 1/2° to 35° at 0.75R; test rig was located outdoors and tests were made under conditions of approximately zero wind velocity; airfoil characteristics computed from statictest data, were considerably different from airfoil characteristics computed from wind tunnel test data.


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    Title :

    Static thrust and power characteristics of six full-scale propellers


    Additional title:

    Nat Advisory Committee Aeronautics -- Report


    Contributors:


    Publication date :

    1940


    Size :

    16 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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