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Free-flight Investigation to Obtain Drag-at-lift and Stability Data for a 60 Degree Delta-wing--body Configuration over a Mach Number Range of 1.3 to 1.6
Clement J. Welsh
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Abstract
Report presenting flight tests using a rocket-propelled 60 degree delta-wing body configuration, which included a NACA 0003-63 wing airfoil section. Drag at lift and stability data were obtained for a range of Mach numbers.