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Force and moment data were botained with a 0.05-scale model of the F-4D aircraft at Mach numbers from 0.75 to l.30 to determine the effects of different store and rack configurations on the static stability and drag of the aircraft. Six proposed rack launchers and four proposed store shapes were tested for a total of 57 external loading configurations. (Author).
Longitudinal aerodynamic characteristics of 0.05-scale models of A-7D and F-4E aircraft were obtained at Mach numbers from 0.50 to 1.30 to determine the effects of store configuration and location on stability and drag. Prototypes, as well as a family of proposed store configurations, were tested. (Author).