Aerodynamic characteristics of a wing with quarter-chord line swept back 60 degrees, aspect ratio 2, taper ratio 0.6, and NACA 65A006 airfoil section : transonic bump method

Author:	Myers, Boyd C., II
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50A12
Link:	https://digital.library.unt.edu/ark:/67531/metadc58424/