Results of studying the aerodynamic performance for a multipurpose medium lift helicopter model are presented. Both integrated and distributed aerodynamic performance of the model is presented along with flow distribution characteristics in the vicinity of the fuselage. The influence of two different rear fuselage geometries on the aerodynamic performance of the fuselage is discussed.


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    Title :

    Investigation of Aerodynamic Performance of a Multipurpose Medium Lift Helicopter with Different Rear Fuselage Geometries


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 64 , 2 ; 248-255


    Publication date :

    2021-04-01


    Size :

    8 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English




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