Experiments were performed with a wing model, to which a rotary cylinder had been fitted. The rotation of the cylinder had a remarkable effect on the aerodynamic properties of the wing.


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    Titel :

    Tests for determining the effect of a rotating cylinder fitted into the leading edge of an airplane wing


    Beteiligte:
    Wolff, E B (Autor:in) / Koning, C (Autor:in)

    Kongress:

    International Congress of Aerial Navigation (3rd : 1925 : Brussels)


    Erscheinungsdatum :

    1926-03-01


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch





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