Investigation at High Subsonic Speeds of the Effect of Adding Various Combinations of Missiles on the Aerodynamic Characteristics of Sweptback and Unswept Wings Combined with a Fuselage
This is a NASA technical report from 1954 on wind-tunnel tests of wing, fuselage and missile combinations at high subsonic speeds, issued for aerodynamics engineers. The three pictures are two dimensioned plan-view drawings of a swept wing with a long fuselage and wing geometry table, and a photograph of a missile model mounted on a sting in the Langley high-speed 7- by 10-foot tunnel. A designer might take from them the clean line-drawing style of technical plans and the crisp contrast of a model shot against a plain tunnel wall.
