ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
Wind tunnel tests were conducted to determine the static stability and control effectiveness of the MK-84 Modular Guided Glide Bomb II MGGB II. A 0.20-scale model of the MK-84 MGGB II was tested at Mach numbers from 0.5 to 1.3 at angles of attack from -12 to 8 deg and sideslip angles from -6 to 14 deg. Aerodynamic coefficients are presented to show the longitudinal, directional, and lateral static stability and control characteristics of the MK-84 MGGB II configuration.
Prepared in cooperation with ARO, Inc., Tullahoma, TN., Rept. no. ARO-PWT-TR-74-42.