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The Use of a Leading-edge Area-suction Flap and Leading-edge Modifications to Improve the High-lift Characteristics of an Airplane Model with a Wing of 45 Degree Sweep and Aspect Ratio 2.8
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Kiyoshi Aoyagi
David G Koenig
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
