Effects of Taper Ratio on the Longitudinal Characteristics at Mach Numbers From 0.6 to 1.4 of a Wing-Body-Tail Combination Having an Unswept Wing of Aspect Ratio 3

Author:	Summers, James L.
Additional Authors:	Treon, Stuart L.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A54L20
Link:	https://digital.library.unt.edu/ark:/67531/metadc61489/