Abstract A technique of evaluating the design parameters for a highly efficient propeller (with optimal geometrical twist) is given. The results of comparative calculations for design parameters of a high-altitude aircraft propeller are presented taking into account air density and compressibility.


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    Title :

    Design of highly efficient propeller blades


    Contributors:

    Published in:

    Publication date :

    2013-04-01


    Size :

    6 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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