May 15 p 80-2, 84. To clarify mechanics of Aeromatic function, analysis of propeller load characteristics is indicated; load curve follows calculated propeller load curve for given non-supercharged engine; this curve is maintained for all flight conditions and altitudes up to critical; however, take-off rpm, function of location of low pitch stop, can be attained whether take-off rating falls on curve or not, in which latter event take-off power is made available by utilizing takeoff rpm and manifold pressure. (See also - n 3 May 1 1944 p 70-3)


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    Title :

    "Aeromatic" propeller makes its debut


    Additional title:

    Aero Digest


    Contributors:
    Fedan, S.H. (author)

    Published in:

    Aero Digest ; 45 , n 4


    Publication date :

    1944


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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