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Effects of canard location on the aerodynamic characteristics of a sharp-nosed missile at Mach numbers of 1.5 and 2.0. [conducted in the Ames 6- by 6-foot wind tunnel

D. L. Kassner, B. Wettlaufer

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Key concepts: Aerodynamics, Wind tunnel, Mach number, Missile, Aerospace engineering, Aeronautics, Meteorology, Marine engineering

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Effects of canard location on the aerodynamic characteristics of a sharp-nosed missile at Mach numbers of 1.5 and 2.0. [conducted in the Ames 6- by 6-foot wind tunnel — Research Paper | ScholarLens