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Experimental Investigation at a Mach Number of 2.41 of Average Skin-friction Coefficients and Velocity Profiles for Laminar and Turbulent Boundary Layers and an Assessment of Probe Effects

Robert M. O'Donnell

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Key concepts: Laminar flow, Mechanics, Parasitic drag, Turbulence, Mach number, Boundary layer, Boundary (topology), Laminar sublayer

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Experimental Investigation at a Mach Number of 2.41 of Average Skin-friction Coefficients and Velocity Profiles for Laminar and Turbulent Boundary Layers and an Assessment of Probe Effects — Research Paper | ScholarLens