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.
Experimental Aerodynamic Characteristics at Mach Numbers from 0.60 to 2.70 of Two Supersonic Cruise Fighter Configurations
1979
190 pages
Report
No indication
English