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Effect of Leading-edge Chord-extensions on the Aerodynamic Characteristics of a 45 Degree Sweptback Wing-fuselage Combination at Mach Numbers of 0.40 to 1.03
Authors
George Liner
Gladys S Martz
F E , Jr West
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
