Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-Chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees

Author:	Kemp, William B., Jr.
Additional Authors:	Goodson, Kenneth W.
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50G14
Link:	https://digital.library.unt.edu/ark:/67531/metadc58552/