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 (1954)
NASA Technical Reports Server (NTRS) · leaf 14
CONFIDENTIAL NACA RM L5lD20 CONFIDENTIAL L-77775 Figiire 5.- Photograph of the test setup in the Langley high-speed 7- hy 10-foot tunnel.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
