Effect of leading-edge sweepback on lift, drag, and pitching-moment characteristics of thin wings of aspect ratio 3 and taper ratio 0.4 at subsonic and supersonic speeds

Author:	Wetzel, Benton E.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A55H04a
Link:	https://digital.library.unt.edu/ark:/67531/metadc61886/