Static Stability and Control Effectiveness of the Super HOBOS/MK-84 (EOGB-II) Munition at Mach Numbers from 0.4 to 1.6
Final rept. 7-19 Jan 1974
ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN
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Wind tunnel tests were conducted on a 0.25-scale model to determine the static stability and control characteristics of the Super HOBOSMK-84 EOGB- II munition. The tests were performed in the Aerodynamic Wind Tunnel 4T over a Mach number range from 0.4 to 1.6 at angles of attack from -4 to 26 deg. Aerodynamic coefficients and control effectiveness data are presented. Two techniques, one using multiple flap deflections and the other single flap deflections, were employed during the test. A comparison of the two methods is presented and the results are discussed.
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