Evaluation of SAGMI and HAST Airloads at the F-4C Centerline Carriage Position for Subsonic and Transonic Mach Numbers
ARO INC ARNOLD AFS TN
Pagination or Media Count:
A wind tunnel investigation was conducted to determine the airloads on the SAGMI and HAST vehicles at the F-4C centerline carriage position. In the process of obtaining these loads, a limited amount of sting interference data on the SAGMI vehicle was obtained. Force and moment data were recorded at Mach numbers from 0.50 to 1.20 for angles of attack from -4 to 12 deg and angles of sideslip from -8 to 8 deg.
- Attack and Fighter Aircraft
- Pilotless Aircraft
- Guided Missile Dynamics, Configurations and Control Surfaces
- Air- and Space-Launched Guided Missiles