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A Flight Investigation of Laminar and Turbulent Boundary Layers Passing Through Shock Waves at Full-scale Reynolds Numbers (1953)

NASA Technical Reports Server (NTRS) · leaf 20

An illustration from A Flight Investigation of Laminar and Turbulent Boundary Layers Passing Through Shock Waves at Full-scale Reynolds Numbers, 1953, leaf 20 — NACA TN 3056 19 Figure 7•- Comparison of the effect of shock waves on the houndary-layer characteristics at low and at high Reynolds numbers with laminar boundary layer ahead of the shock wave.

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