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Distribution of lift and pitching moment between wing and fuselage and effects of wing flexibility and dive brake on a 1/30-scale semispan model of the Bell X-5 airplane at transonic speeds as determined by the NACA wing-flow method

Garland J Morris, Norman S Silsby

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Key concepts: Fuselage, Wing, Airplane, Wing configuration, Lift (data mining), Aerospace engineering, Wing loading, Wing twist

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Distribution of lift and pitching moment between wing and fuselage and effects of wing flexibility and dive brake on a 1/30-scale semispan model of the Bell X-5 airplane at transonic speeds as determined by the NACA wing-flow method — Research Paper | ScholarLens