Aerodynamic characteristics of a wing with quarter-chord line swept back 45 degrees, aspect ratio 6, taper ratio 0.6, and NACA 65A009 airfoil section

Author:	Spreemann, Kenneth P.
Additional Authors:	Morrison, William D., Jr.
Year:	1949
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50B03a
Link:	https://digital.library.unt.edu/ark:/67531/metadc58527/