Preliminary Report on Laminar-Flow Airfoils and New Methods Adopted for Airfoil and Boundary-Layer Investigations (1939)
NASA Technical Reports Server (NTRS) · leaf 28
41 3 4 5 6 ?8 Reynolds number, millions Figure 5,- Method of transition measurement. Variation of the "transition function" and correlation with hot-wire studies.
NASA Technical Reports Server (NTRS)
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