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An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback : Force Characteristics of the Complete Configuration and Its Various Components at Mach Numbers of 1.40 and 1.59
Norman F. Smith, J. E. Marte
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Abstract
Report presenting an investigation of a supersonic aircraft configuration and various combinations of its components at a range of Mach numbers. Longitudinal- and lateral-force characteristics of the configurations, as well as longitudinal- and lateral-stability derivatives, are provided.