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Wind-tunnel investigation of the flow correction for a model-mounted angle of attack sensor at angles of attack from -10 deg to 110 deg. [Langley 12-foot low speed wind tunnel test]

T. M. Moul

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Key concepts: Wind tunnel, Angle of attack, Supersonic wind tunnel, Flow (mathematics), Marine engineering, Mechanics, Meteorology, Engineering

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Wind-tunnel investigation of the flow correction for a model-mounted angle of attack sensor at angles of attack from -10 deg to 110 deg. [Langley 12-foot low speed wind tunnel test] — Research Paper | ScholarLens