TESTS IN THE PWT 16-FT TRANSONIC CIRCUIT OF AN AGARD MODEL B AND A MODIFIED MODEL C AT 1.15-PERCENT BLOCKAGE

摘要

Lift, drag, and pitching moment characteristics of the AGARD Model B and a modified AGARD Model C were obtained at the AEDC in the 16-Ft Transonic Circuit of the Propulsion Wind Tunnel Facility. The Mach number was varied from 0.70 to 1.60 and the angle of attack from -4 to +9 degrees. The models represented 1.15-percent blockage. The Reynolds number based on the wing mean aerodynamic chord was approximately 10 x 106.