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Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-wing Fighter-bomber-type Airplane with a Top Inlet at Mach Numbers from 1.6 to 2.35

A. V. Gnos, R. L. Kurkowski

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

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Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-wing Fighter-bomber-type Airplane with a Top Inlet at Mach Numbers from 1.6 to 2.35 — Research Paper | ScholarLens