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aerodynamic aileron deflection aileron profile airfoil airfoil section altitude angle of attack angle of yaw approximately beveled ailerons blade angle blade section boundary layer calculations characteristics chord COMMITTEE FOR AERONAUTICS comparison compression ratio computed curves decrease density drag coefficient duct effects equation experimental feet figure of merit flap flight front spar fuel rate Hamilton Standard inch increase indicated internal flow investigation jet-propulsion system Langley Field Langley Memorial Aeronautical lift coefficient low-drag wing Mach number Martin Company mass-flow maximum measured Memorial Aeronautical Laboratory miles per hour NACA NATIONAL ADVISORY COMMITTEE o o o obtained outlet panel percent power conditions pressure drop profile drag propeller propeller operation propulsion radiator range reduced Reynolds number rudder saiavaan seal shown in figure skin joints speed static thrust station take-off temperature tests thermal efficiency tip-speed ratio trailing edge tube tunnel upper surface variation velocity WARTIME REPORT wind-tunnel