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Low-speed pressure-distribution investigation of a spoiler and a spoiler-slot-deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section

Alexander D Hammond

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Key concepts: Fuselage, Aspect ratio (aeronautics), Wing, Overall pressure ratio, Degree (music), Structural engineering, Materials science, Acoustics

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Low-speed pressure-distribution investigation of a spoiler and a spoiler-slot-deflector on a 30 degree sweptback wing-fuselage model having an aspect ratio of 3, a taper ratio of 0.5, and NACA 65A004 airfoil section — Research Paper | ScholarLens