Longitudinal stability and control characteristics at Mach numbers of 1.41 and 2.01 of a 67 degree swept-wing airplane configuration with canard control surfaces

Author:	Spearman, M. Leroy
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L58E20
Link:	https://digital.library.unt.edu/ark:/67531/metadc64251/