The lift distribution of wings with end plates
This is a 1938 NACA technical memorandum, issued by a US aeronautical research body, on the lift distribution of wings fitted with end plates, presented as engineering graphs for aircraft designers and aerodynamicists. The pictures are plotted curves and charts of circulation, side force and moment coefficients against parameters such as end plate height ratio and angle of attack, with labelled families of lines on gridded axes, offering a designer little beyond the data trends themselves.
