Low speed flow angularity results are presented showing flow direction at the nacelle locations on the Boeing 727-200. Flow angle probes (yawheads) were used for measurements at side and center inlet positions on the aft fuselage. A range of flap settings were tested with flap angles of 0 deg, 15 deg, and 40 deg selected for investigation. (Author)


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    Titel :

    Low Speed Wind Tunnel Flow Field Results for Jt8d Refan Engines on the Boeing 727-200


    Beteiligte:
    W. G. Easterbrook (Autor:in) / W. H. Roberts (Autor:in)

    Erscheinungsdatum :

    1974


    Format / Umfang :

    25 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch