Aerodynamic characteristics at subcritical and supercritical Mach numbers of two airfoil sections having sharp leading edges and extreme rearward positions of maximum thickness

Author:	Eggers, A. J., Jr.
Year:	1947
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A7C10
Link:	https://digital.library.unt.edu/ark:/67531/metadc58030/