Wind Tunnel Tests on a Model of a Monoplane Wing with Floating Ailerons
This is a 1929 NACA technical report, issued by the National Advisory Committee for Aeronautics, presenting wind tunnel measurements on a model monoplane wing fitted with floating ailerons, written for aeronautical engineers. The pictures are plotted graphs of lift and drag coefficients and rolling moment curves, with a line drawing and photograph of the rolling and yawing moment balance; a designer might take from them the clean, gridded plotting style with labelled curves and small symbol markers.
