Determination of the theoretical pressure distribution for twenty airfoils
A 1934 NASA Technical Reports Server publication, issued by the National Advisory Committee for Aeronautics, presenting calculated theoretical pressure distributions for twenty airfoil sections for aircraft wing design. Its pictures are engineering line graphs of pressure against percent chord, plotted as smooth upper and lower surface curves beside profile drawings of the airfoil shapes, offering a designer clean, sparse linework with dense labelled axes and captions.
