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Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 deg delta wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70

Aleck C. Bond, Andrew Swanson

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Key concepts: Mach number, Longitudinal static stability, Aerospace engineering, Delta wing, Aeronautics, Duct (anatomy), Wing, Angle of attack

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Rocket-model investigation of the longitudinal stability, drag, and duct performance of a 60 deg delta wing canard aircraft with twin side inlets at Mach numbers from 0.80 to 1.70 — Research Paper | ScholarLens