The Effect of Changes in the Leading-Edge Radius on the Aerodynamic Characteristics of a Symmetrical, 9-Percent-Thick Airfoil at High-Subsonic Mach Numbers

Author:	Humphreys, Milton D.
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L9L09
Link:	https://digital.library.unt.edu/ark:/67531/metadc58458/