1971•Unpublished venueRequires access

Measurements of the boundary layer and wake of two aerofoil sections at high Reynolds numbers and high-subsonic Mach numbers

T. A. Cook

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Key concepts: Wake, Reynolds number, Boundary layer, Mach number, Airfoil, Mechanics, Mathematics, Physics

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Measurements of the boundary layer and wake of two aerofoil sections at high Reynolds numbers and high-subsonic Mach numbers — Research Paper | ScholarLens