Flight investigation to determine aerodynamic characteristics of propeller at forward Mach numbers up to about 0.95; efficiency is approximately 79% at Mach number of 0.948 and advance ratio of 3.5.


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    Title :

    Effect of advance ratio on flight performance of modified supersonic propeller


    Additional title:

    NACA -- Tech Note


    Contributors:

    Published in:

    Publication date :

    1958


    Size :

    20 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :