Transonic Wind-Tunnel Investigation of the Effect of Horizontal Tail on Longitudinal Stability of Two 60 Degree Sweptback-Wing-Body Configurations with Aspect Ratios of 2.67 and 4.00

Author:	Brooks, Joseph D.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57L11
Link:	https://digital.library.unt.edu/ark:/67531/metadc64355/