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Effect of Vertical Location of a Horizontal Tail on the Static Longitudinal Stability Characteristics of a 45 Degree Sweptback-wing-fuselage Combination of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)

Reino J Salmi, William A Jacques

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Key concepts: Wing, Fuselage, Aspect ratio (aeronautics), Reynolds number, Degree (music), Longitudinal static stability, Geometry, Horizontal and vertical

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Effect of Vertical Location of a Horizontal Tail on the Static Longitudinal Stability Characteristics of a 45 Degree Sweptback-wing-fuselage Combination of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6) — Research Paper | ScholarLens