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.


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    Title :

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


    Contributors:

    Publication date :

    1979


    Size :

    190 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English