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Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Characteristics at Supersonic Speeds of a Model with the Wing Twisted and Cambered for Uniform Load

Charles Francis Hall, John C Heitmeyer

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Key concepts: Wing, Fuselage, Aerodynamics, Wing twist, Wing configuration, Wing loading, Supersonic speed, Aerospace engineering

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Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Characteristics at Supersonic Speeds of a Model with the Wing Twisted and Cambered for Uniform Load — Research Paper | ScholarLens