The effects of compressibility on the lift, pressure, and load characteristics of a tapered wing of NACA 66-series airfoil sections

Author:	Cooper, Morton
Year:	1948
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1697
Link:	https://digital.library.unt.edu/ark:/67531/metadc54797/