Lift, drag, and static longitudinal stability characteristics of four airplane-like configurations at Mach numbers from 3.00 to 6.28

Author:	Neice, Stanford E.
Additional Authors:	Wong, Thomas J.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A55C24
Link:	https://digital.library.unt.edu/ark:/67531/metadc61429/