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STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS

Cornelius Driver, M Leroy Spearman

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Abstract

Stability and control of supersonic vtol airplane model having broad fuselage and small delta wing

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Stability and control of supersonic vtol airplane model having broad fuselage and small delta wing

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Available abstract

Stability and control of supersonic vtol airplane model having broad fuselage and small delta wing

Key concepts: Fuselage, Airplane, Supersonic speed, Mach number, Delta wing, Aeronautics, Aerospace engineering, Flight control surfaces

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STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGS — Research Paper | ScholarLens