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High Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 1/16-Scale Model of the D-558-2 Research Airplane at High Subsonic Mach Number and at a Mach Number of 1.2

Robert S. Osborne

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Key concepts: Airplane, Mach number, Wind tunnel, Aerospace engineering, Longitudinal static stability, Scale (ratio), Stability (learning theory), Aerodynamics

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High Speed Wind-Tunnel Investigation of the Longitudinal Stability and Control Characteristics of a 1/16-Scale Model of the D-558-2 Research Airplane at High Subsonic Mach Number and at a Mach Number of 1.2 — Research Paper | ScholarLens