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Longitudinal characteristics at Mach Number of 1.24 of 1/30-scale semispan model of Bell X-5 variable-sweep airplane with wing swept back 60 degrees : from tests by NACA wing-flow method

Norman S Silsby, Garland J Morris, Robert M. Kennedy

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Key concepts: Wing, Airplane, Wing configuration, Mach number, Wing loading, Swept wing, Variable (mathematics), Scale (ratio)

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Longitudinal characteristics at Mach Number of 1.24 of 1/30-scale semispan model of Bell X-5 variable-sweep airplane with wing swept back 60 degrees : from tests by NACA wing-flow method — Research Paper | ScholarLens