Effects of independent variations of mach number and reynolds number on the maximum lift coefficients of four NACA 6-series airfoil sections

Author:	Racisz, Stanley F.
Year:	1952
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2824
Link:	https://digital.library.unt.edu/ark:/67531/metadc56326/