An evaluation of the characteristics of a 10-percent-thick NACA 66-series airfoil section with a special mean-camber line designed to produce a high critical Mach number

Author:	Loftin, Laurence K., Jr.
Year:	1948
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1633
Link:	https://digital.library.unt.edu/ark:/67531/metadc54726/