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Wind-tunnel investigation at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control. [in the Langley Unitary Plan Wind Tunnel

A. B. Blair

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Key concepts: Wind tunnel, Mach number, Missile, Aeronautics, Aerospace engineering, Engineering, Jet (fluid), Supersonic wind tunnel

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Wind-tunnel investigation at Mach numbers from 1.90 to 2.86 of a canard-controlled missile with ram-air-jet spoiler roll control. [in the Langley Unitary Plan Wind Tunnel — Research Paper | ScholarLens