Effects of Reynolds number and leading-edge shape on the low-speed longitudinal stability of a 6-percent-thick 45 degree sweptback wing

Author:	Schneider, William C.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L56B14
Link:	https://digital.library.unt.edu/ark:/67531/metadc62251/