The dependences of the defining coefficients of the blade operation on various environmental conditions are considered. The best airfoil of the blade with high efficiency in a wide range of operating conditions is determined.


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    Title :

    Selection of the Optimal Airfoil for the Small-Sized Unmanned Helicopter Main Rotor Blade


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 65 , 3 ; 524-532


    Publication date :

    2022-07-01


    Size :

    9 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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