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Static and Dynamic-rotary Stability Derivatives of an Airplane Model with an Unswept Wing and a High Horizontal Tail at Mach Numbers of 2.5, 3.0, and 3.5

B. A. Lampkin, Phillips J Tunnell

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Key concepts: Wing, Airplane, Longitudinal static stability, Mach number, Stability (learning theory), Wing loading, Stability derivatives, Engineering

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Static and Dynamic-rotary Stability Derivatives of an Airplane Model with an Unswept Wing and a High Horizontal Tail at Mach Numbers of 2.5, 3.0, and 3.5 — Research Paper | ScholarLens