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EFFECT OF VERTICAL-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS

Ross B Robinson, M Leroy Spearman

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Key concepts: Fuselage, Supersonic speed, Airplane, Mach number, Delta wing, Longitudinal static stability, Aerospace engineering, Stability (learning theory)

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EFFECT OF VERTICAL-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS — Research Paper | ScholarLens