ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
A wind tunnel test was conducted using 0.05-scale models to study the separation characteristics of the SUU-51B from the F-4C aircraft. The separation trajectories were initiated from the left-wing inboard pylon station utilizing the Triple Ejection Rack and from the centerline pylon utilizing the Multiple Ejection Rack. The flight conditions simulated were Mach numbers from 0.66 to 0.90 at an altitude of 5000 ft. Parent aircraft dive angles of 0, 30, and 45 deg were simulated.
Prepared in cooperation with ARO, Inc., Tullahoma, TN., Rept. no. ARO-PWT-TR-71-104.