In order to determine the maximum and the most favorable pitch for a propeller, it was found desirable to investigate the dependence of propeller efficiency on the angle of attack of the propeller blade. The results of a few experiments are given to show that propeller blades conduct themselves just like airplane wings with reference to the dependence of their efficiency on their angle of attack.


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    Title :

    Dependence of propeller efficiency on angle of attack of propeller blade


    Contributors:

    Publication date :

    1921-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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