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Flight-determined static lateral stability and control characteristics of a swept-wing fighter airplane to a Mach number of 1.39

G. J. Matranga, James R Peele

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Key concepts: Airplane, Wing, Longitudinal static stability, Mach number, Aerospace engineering, Wing configuration, Flight control surfaces, Aeronautics

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Flight-determined static lateral stability and control characteristics of a swept-wing fighter airplane to a Mach number of 1.39 — Research Paper | ScholarLens