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Aerodynamic Characteristics of a Wing with Quarter-chord Line Swept Back 35 Degrees, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006 Airfoil Section : Transonic-bumb Method
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Robert E Becht
William C , Jr Sleeman
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oai:casi.ntrs.nasa.gov:1993008...
Last time updated on 03/08/2016
