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Longitudinal and lateral stability characteristics of a low-aspect-ratio unswept-wing airplane model at Mach numbers of 1.82 and 2.01

M Leroy Spearman, Cornelius Driver

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Key concepts: Airplane, Wing, Longitudinal static stability, Mach number, Aerospace engineering, Stability (learning theory), Wing loading, Aeronautics

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Longitudinal and lateral stability characteristics of a low-aspect-ratio unswept-wing airplane model at Mach numbers of 1.82 and 2.01 — Research Paper | ScholarLens