Investigation of the Effects of Wing and Tail Modifications on the Low-Speed Stability Characteristics of a Model Having a Thin 40 Degree Swept Wing of Aspect Ratio 3.5

Author:	Weil, Joseph
Additional Authors:	Sleeman, William C., Jr.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53C09
Link:	https://digital.library.unt.edu/ark:/67531/metadc59733/