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Flow visualization studies of a general research fighter model employing a strake-wing concept at subsonic speeds. [in the Langley high speed 7- by 10-ft wind tunnel

James M. Luckring

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Key concepts: Wind tunnel, Flow visualization, Wing, Flow (mathematics), Aerodynamics, Marine engineering, Swept wing, Geology

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Flow visualization studies of a general research fighter model employing a strake-wing concept at subsonic speeds. [in the Langley high speed 7- by 10-ft wind tunnel — Research Paper | ScholarLens