Exploratory investigation at high and low subsonic Mach numbers of two experimental 6-percent-thick airfoil sections designed to have high maximum lift coefficients

Author:	Loftin, Laurence K., Jr.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51F06
Link:	https://digital.library.unt.edu/ark:/67531/metadc64978/