Static lateral stability and control characteristics of a model of a 45 degree swept-wing fighter airplane with various vertical tails at Mach numbers of 1.41, 1.61, and 2.01

Author:	Spearman, M. Leroy
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L56D05
Link:	https://digital.library.unt.edu/ark:/67531/metadc62571/