The aerodynamic design of propellers from considerations of centrifugal force is presented. A solution is obtained for the span wise distribution of cross-sectional area required to attain constant centrifugal stress over most of the blade.


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    Title :

    Aerodynamic Design of Supersonic Propellers From Structural Considerations


    Contributors:

    Publication date :

    1952


    Size :

    23 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English