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Aerodynamic characteristics of a canard-controlled missile at Mach numbers of 0.8, 1.3, and 1.75. [in the Ames 6 by 6 foot wind tunnel]

D. L. Kassner, B. Wettlaufer

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Key concepts: Mach number, Aerodynamics, Wind tunnel, Aeronautics, Missile, Aerospace engineering, Foot (prosody), Engineering

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Aerodynamic characteristics of a canard-controlled missile at Mach numbers of 0.8, 1.3, and 1.75. [in the Ames 6 by 6 foot wind tunnel] — Research Paper | ScholarLens