Two 0.085-scale full span wind-tunnel models of a Mach 1.60 design supercruiser configuration were tested at Mach numbers from 0.60 to 2.70. One model incorporated a varying dihedral (swept-up) wing to obtain the desired lateral-directional characteristics; the other incorporated more conventional twin vertical tails. The data from the wind-tunnel tests are presented without analysis.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Experimental Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.70 of Two Supersonic Cruise Fighter Configurations


    Beteiligte:

    Erscheinungsdatum :

    1979


    Format / Umfang :

    190 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch