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Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effect of Reynolds Number at Supersonic Mach Numbers on the Longitudinal Characteristics of a Wing Twisted and Cambered for Uniform Load

By John C Heitmeyer
Year: 1950
OAI identifier: oai:casi.ntrs.nasa.gov:19930086361
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