Subsonic Aerodynamic Characteristics up to Extreme Angles of Attack of an Airplane Model Having an Unswept Wing and a High Horizontal Tail
This is a NASA technical report from 1958 on wind-tunnel tests of an airplane model with an unswept wing and high horizontal tail at extreme angles of attack, written for aeronautical engineers. Its pictures are plain line graphs with dense gridded axes, plotting pitching moment and lift coefficients against angle in degrees with labelled curve sets and point markers, offering a designer little beyond the restrained scientific chart vocabulary of its period.
