The propulsive airfoil is investigated by determining the optimum air flow rate taken from the surface and comparing it with the air flow rate of the engines installed on the helicopter. The lift force generated by the developed airfoil is compared with the helicopter launch weight.


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    Title :

    Study of Aerodynamics of Propulsive Helicopter Fuselage


    Additional title:

    Russ. Aeronaut.


    Contributors:

    Published in:

    Russian Aeronautics ; 66 , 3 ; 493-499


    Publication date :

    2023-08-01


    Size :

    7 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English






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