Tests in the variable-density wind tunnel of related airfoils having the maximum camber unusually far forward
This is a 1936 NACA technical report of wind tunnel test results for airfoils with maximum camber placed far forward, issued by the National Advisory Committee for Aeronautics for aeronautical engineers and researchers. The pictures are dense engineering graphs with gridded plots of lift and drag coefficients, centre of pressure curves, and airfoil cross-section profiles, offering a designer rigid grid-plotting layouts, precise curve styling, and clean technical typography.
