The trajectories of droplets in the air flowing past an NACA 65AO04 airfoil at an angle of attack of 8 deg were determined.. The amount of water in droplet form impinging on the airfoil, the area of droplet impingement, and the rate of droplet impingement per unit area on the airfoil surface were calculated from the trajectories and presented to cover a large range of flight and atmospheric conditions. These impingement characteristics are compared briefly with those previously reported for the same airfoil at an angle of attack of 4 deg.


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    Titel :

    Impingement of Water Droplets on NACA 65A004 Airfoil at 8 deg Angle of Attack


    Beteiligte:
    Brun, R. J. (Autor:in) / Gallagher, H. M. (Autor:in) / Vogt, D. E. (Autor:in)

    Erscheinungsdatum :

    01.07.1954


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Impingement of water droplets on NACA 65a004 airfoil at 0° angle of attack

    Brun, R.J. / Vogt, D.E. | Engineering Index Backfile | 1955


    Impingement of water droplets on NACA 65A004 airfoil at 8 [degrees] angle of attack

    Brun, Rinaldo J. / Gallagher, Helen M. / Vogt, Dorothea E. | TIBKAT | 1954



    Impingement of water droplets on NACA 65a004 airfoil at 8° angle of attack

    Brun, R.J. / Gallagher, H.M. / Vogt, D.E. | Engineering Index Backfile | 1954