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Effects of Spanwise Thickness Variation on the Aerodynamic Characteristics of 35 Deg. and 45 Deg. Swept Back Wings of Aspect Ratio 6 Transonic-bump Method

Lewis E. Wallner, John T Wintler

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Key concepts: Transonic, Aerodynamics, Swept wing, Variation (astronomy), Wing, Angle of attack, Aspect ratio (aeronautics), Materials science

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Effects of Spanwise Thickness Variation on the Aerodynamic Characteristics of 35 Deg. and 45 Deg. Swept Back Wings of Aspect Ratio 6 Transonic-bump Method — Research Paper | ScholarLens