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Effects of Spanwise Thickness Variation on the Aerodynamic Characteristics of 35 Degree and 45 Degree Sweptback Wings of Aspect Ratio 6 : Transonic-bump Method

William D Morrison, P. G. Fournier

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Key concepts: Degree (music), Transonic, Aerodynamics, Variation (astronomy), Mathematics, Aspect ratio (aeronautics), Geometry, Materials science

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Effects of Spanwise Thickness Variation on the Aerodynamic Characteristics of 35 Degree and 45 Degree Sweptback Wings of Aspect Ratio 6 : Transonic-bump Method — Research Paper | ScholarLens