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Collection and Summary of Flap-type-aileron Rolling-effectiveness Data at Zero Lift as Determined by Rocket-powered Model Tests at Mach Numbers Between 0.6 and 1.6
Authors
E M Fields
Eugene D Schult
Emily W Stephens
H Kurt Strass
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
