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Wind-tunnel Investigation at Mach Numbers from 0.50 to 1.29 of an Unswept, Tapered Wing of Aspect Ratio 2.67 with Leading- and Trailing-edge Flaps - Leading-edge Flaps Deflected
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Alexander W Malick
Louis S , Jr Stivers
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
