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Large-scale Wind-tunnel Tests of an Airplane Model with a 45 Degree Sweptback Wing of Aspect Ratio 2.8 Employing High-velocity Blowing over the Leading- and Trailing-edge Flaps
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Kiyoshi Aoyagi
David H Hickey
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
