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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 12

An illustration from 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, leaf 12
12 NACA RM L5LD20 CONFIDENTIAL — Sting 2.63 … Figure 1.- Drawing of the swept-wing model. CONFIDENTIAL

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