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Lift, Drag, and Longitudinal Stability at Mach Numbers from 1.4 to 2.3 of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces
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Warren, Jr Gillespie
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
