Effects of spanwise thickness variation on the aerodynamic characteristics of 35 degree and 45 degree sweptback wings of aspect ratio 6: transonic-bump method

Author:	Morrison, William D., Jr.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51D19
Link:	https://digital.library.unt.edu/ark:/67531/metadc58795/