The results of experimental studies of the effect of relative curvature of the airfoils on the degree
    of change in their characteristics in terms of additional pulse velocity in the boundary layer top
    surface profile generated by a rotating cylinder. It was found that the growth profile of the greater
    curvature of the lift coefficient in the linear region up to increase the lift coefficient by the
    application of flap - the flap


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    Title :

    RESULTS OF EXPERIMENTAL RESEARCHES OF FLOWING AROUND AEROFOIL IN PRESENCE THE REVOLVED CYLINDER


    Contributors:


    Publication date :

    2011




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




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