Aerodynamic characteristics of a wing with quarter-chord line swept back 35 degrees, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section : transonic-bumb method

Author:	Sleeman, William C , Jr
Year:	1949
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L9B25
Link:	https://digital.library.unt.edu/ark:/67531/metadc58209/