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The effects of horizontal-tail location and size on the subsonic longitudinal aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3

Bruce E Tinling, Armando E. Lopez

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Key concepts: Airplane, Wing, Aerodynamics, Aspect ratio (aeronautics), Aerospace engineering, Geology, Physics, Engineering

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The effects of horizontal-tail location and size on the subsonic longitudinal aerodynamic characteristics of an airplane model having a triangular wing of aspect ratio 3 — Research Paper | ScholarLens