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 at M

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National Advisory Committee for Aeronautics, 1952 - Aerodynamics, Supersonic - 27 pages
 

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