Longitudinal Stability and Drag Characteristics at Mach Numbers From 0.75 to 1.5 of an Airplane Configuration Having a 60 Degree Swept Wing of Aspect Ratio 2.24 as Obtained From Rocket-Propelled Models

Author:	Vitale, A. James
Additional Authors:	McFall, John C., Jr.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51K06
Link:	https://digital.library.unt.edu/ark:/67531/metadc59274/