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Effects of Systematically Varying the Spanwise and Vertical Location of an External Store on the Aerodynamic Characteristics of an Unswept Tapered Wing of Aspect Ratio 4 at Mach Numbers of 1.41, 1.62, and 1.96

Carl R Jacobsen

Abstract

Report presenting an investigation in the supersonic blowdown tunnel to determine the effects of an external store on the lift, drag, and pitching-moment characteristics of an unswept wing of aspect ratio 4 at Mach numbers of 1.41, 1.62, and 1.96.

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Key concepts: Mach number, Aerodynamics, Lift-induced drag, Wing, Boiler blowdown, Drag divergence Mach number, Drag, Lift (data mining)