Investigation of Boundary-Layer Reynolds Number for Transition on NACA 65 215)=114 Airfoil in Langley Two-Dimensional Low-Turbulence Pressure Tunnel.
Investigation of boundary-layer Reynolds number for transition on NACA 65 215)=114 airfoil in Langley two-dimensional low-turbulence pressure tunnel
Nat Advisory Committee Aeronautics -- Tech Note
1948
22 pages
Report
Englisch
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