Investigation of Boundary-Layer Reynolds Number for Transition on an NACA 65 (Sub 215)-114 Airfoil in the Langley Two-Dimensional Low-Turbulence Pressure Tunnel

Author:	Braslow, Albert L.
Year:	1948
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NASA-TM-79859, NACA-TN-1704
Link:	https://digital.library.unt.edu/ark:/67531/metadc53353/