Consequences of dimensional deviations of actual blades from those of assumed standard are examined, and apparatus devised to minimize or eliminate most undesirable of them, namely, tendency to induce vibration in aircraft, is described.


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    Title :

    Aerodynamic balancing of propellers


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:

    Published in:

    Publication date :

    1949


    Size :

    14 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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