Distribution of Pressure Over Model of the Upper Wing and Aileron of a Fokker D-VII Airplane
This is a 1927 NASA technical report on pressure distribution across a model of a Fokker D-VII upper wing and aileron, issued by the National Advisory Committee for Aeronautics for engineers and aerodynamicists. The pictures are plates of dense flow-line diagrams and pressure curves plotted over wing sections, with aileron deflection and angle of attack labelled under each panel; a designer might borrow their clean line-work and stacked small-multiple layout.
