Analytical determination of the load on a trailing edge flap
A 1930 NACA technical note from the NASA Technical Reports Server, presenting an analytical method for the aerodynamic load on a trailing edge flap, aimed at aeronautical engineers. The single figure is a graph of theoretical parameters plotted against the ratio of flap chord to total chord, with a small airfoil sketch above showing airflow and deflection. Its plain black linework, grid and labelled axes suit a designer wanting a technical diagram vocabulary of precise measured charts.
