Wind-tunnel tests of a full-scale model of the Republic XF-91 airplane were conducted to determine the distribution of pressure over the external wing fuel tank installation and over the vee tail and ventral fin. The data were obtained for a range of angles of attack and sideslip and elerudder deflection angles; the presentation is in tabular form.


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    Titel :

    An Investigation of a Full-Scale Model of the Republic XF-91 Airplane in the Ames 40- By 80-Foot Wind Tunnel: Pressure Data


    Beteiligte:
    Hunton, Lynn W. (Autor:in) / Dew, Joseph K. (Autor:in)

    Erscheinungsdatum :

    25.03.1949


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch