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Longitudinal Stability and Control Characteristics at Transonic Speeds of a Semispan Airplane Model Having a 45 Degree Sweptback Wing and Tail as Obtained by the Transonic-bump Method

Leroy Spearman

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Key concepts: Transonic, Airplane, Wing, Degree (music), Stability (learning theory), Longitudinal static stability, Aeronautics, Aerospace engineering

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Longitudinal Stability and Control Characteristics at Transonic Speeds of a Semispan Airplane Model Having a 45 Degree Sweptback Wing and Tail as Obtained by the Transonic-bump Method — Research Paper | ScholarLens