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The static and dynamic-rotary stability derivatives of a model of the x-15 research airplane at mach numbers from 1.55 to 3.50

Eldon A. Latham, Phillips J Tunnell

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Key concepts: Airplane, Mach number, Stability (learning theory), Longitudinal static stability, Aerospace engineering, Engineering, Aeronautics, Computer science

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The static and dynamic-rotary stability derivatives of a model of the x-15 research airplane at mach numbers from 1.55 to 3.50 — Research Paper | ScholarLens