Effects of vertical location of wing and horizontal tail on the aerodynamic characteristics in pitch at Mach numbers from 0.60 to 1.40 of an airplane configuration with an unswept wing

Author:	Stivers, Louis S , Jr
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A57I10
Link:	https://digital.library.unt.edu/ark:/67531/metadc64247/