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Lateral Stability Investigation at Mach Numbers from 0.8 to 1.7 of Two Rocket-boosted Models of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail

John C Mcfall, Jesse L Mitchell, Antonio Vitale

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Key concepts: Airplane, Aerospace engineering, Mach number, Wing, Longitudinal static stability, Degree (music), Rocket (weapon), Aeronautics

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Lateral Stability Investigation at Mach Numbers from 0.8 to 1.7 of Two Rocket-boosted Models of an Airplane Configuration with a 45 Degree Swept Wing and a Low Horizontal Tail — Research Paper | ScholarLens