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Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of a canard missile configuration

J Richard Spahr, R. A. Robinson

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Key concepts: Mach number, Aerospace engineering, Missile, Wind tunnel, Aeronautics, Engineering, Meteorology, Physics

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Wind-tunnel investigation at Mach numbers of 1.5 and 2.0 of a canard missile configuration — Research Paper | ScholarLens