Effects of some leading-edge modifications, section and plan-form variations, and vertical position on low-lift wing drag at transonic and supersonic speeds
Description: Report presents information about free-flight rocket-propelled model testing to determine the effect of some wing geometry variables on low lift drag at a range of Mach numbers. Results regarding the effect of airfoil section, wing nose droop and nose flaps, plan form, and wing vertical position are provided.
Date: January 18, 1955
Creator: Welsh, Clement J.; Wallskog, Harvey A. & Sandahl, Carl A.
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Partner: UNT Libraries Government Documents Department