Oil flow on the surface and pitot pressure measurements in the wake of a 0.762 m chord airfoil in a 8 ft x 6 ft tunnel indicate that there is no significant spanwise convergence or divergence of the flow within the boundary layer and wake of the model. The measurements were made at subsonic conditions where no regions of separated flow existed on the model, but where significant subsonic drag creep had previously been measured.


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    Titel :

    A Brief Investigation of the Two-Dimensionality of the Flow over an Airfoil in the 8 Foot by 6 Foot Transonic Wind Tunnel


    Beteiligte:
    P. H. Cook (Autor:in) / M. A. Mcdonald (Autor:in)

    Erscheinungsdatum :

    1979


    Format / Umfang :

    20 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch