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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    Titel :

    Dependence of propeller efficiency on angle of attack of propeller blade


    Beteiligte:
    Borck, Hermann (Autor:in)

    Erscheinungsdatum :

    01.01.1921


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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