Interference of Wing and Fuselage from Tests of 209 Combinations in the NACA Variable-Density Tunnel
This is an NACA technical report from 1936 by the National Advisory Committee for Aeronautics, published as a NASA Technical Reports Server item, presenting wind-tunnel test data on how wings and fuselages interact across 209 model configurations. Its pictures are black-and-white photographs of a model balance inside the tunnel, a plate of streamlined fuselage and wing-fillet profiles, and a graph of lift coefficient against drag and pitching moment, which a designer might draw on for clean technical diagram layouts and restrained grayscale plate design.
