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aerodynamic characteristics AERONAUTICS TECHNICAL NOTE airfoil airfoil section airplane angle of attack approximately aspect ratio Battelle ref blade boundary layer calculated camber chord COMMITTEE FOR AERONAUTICS components correlation function crossflow curves dead-air pressure deflection determined dissociation downstream drag coefficient effects end plates equation experimental Fatigue free-stream frequency fuselage hypersonic increase inertia investigation jet flap jet-augmented KN OJ knife edges Langley Langley Aeronautical Laboratory Langley Field leading-edge lift coefficient Mach number maximum measured mode momentum coefficient NACA TN NATIONAL ADVISORY COMMITTEE obtained OJ OJ P-VO parameter plotted pressure coefficient pressure distribution pressure rise pure laminar separations reaction reattachment reference Reynolds number separated flow shadowgraphs shock wave shown in figure sketch solution span specimens speed stagnation pressure streamline stress structural damping Subresonant machines subsonic supersonic taper ratio theory tion transition location transonic turbulent separation two-dimensional UNVO upstream values variation velocity wind tunnel wing wing-fuselage zero