Effect of compressibility on normal-force, pressure, and load characteristics of a tapered wing of NACA 66-series airfoil sections with split flaps

Author:	West, F E
Year:	1948
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1759
Link:	https://digital.library.unt.edu/ark:/67531/metadc54984/