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Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 : Effects of Sweep Angle and Thickness Ratio on the Aerodynamic Characteristics in Pitch

Cornelius Driver, Ross B Robinson

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Key concepts: Wing, Supersonic speed, Aerodynamics, Aspect ratio (aeronautics), Series (stratigraphy), Wing loading, Angle of attack, Mechanics

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Aerodynamic Characteristics at Supersonic Speeds of a Series of Wing-body Combinations Having Cambered Wings with an Aspect Ratio of 3.5 and a Taper Ratio of 0.2 : Effects of Sweep Angle and Thickness Ratio on the Aerodynamic Characteristics in Pitch — Research Paper | ScholarLens