Wind-tunnel research comparing lateral control devices, particularly at high angles of attack I : ordinary ailerons on rectangular wings
A 1933 NASA technical report, issued through the NASA Technical Reports Server, presents wind-tunnel research comparing aileron designs for airplane lateral control at high angles of attack. Its pictures are engineering graphs of rolling and yawing moment coefficients plotted against angle of attack, plus diagrams of aileron deflection arrangements, offering a designer sparse technical line work with dashed and solid curves and labelled axes.
