Longitudinal Stability and Wake-Flow Characteristics of a Twisted and Cambered Wing-Fuselage Combination of 45 Degree Sweepback and Aspect Ratio 8 With a Horizontal Tail and Stall-Control Devices at a Reynolds Number of 4.0 X 10 (Exp 6)

Author:	Foster, Gerald V.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53D08
Link:	https://digital.library.unt.edu/ark:/67531/metadc59790/