Static longitudinal stability and control characteristics of a model of a 45 degree swept-wing fighter airplane at Mach numbers of 1.41, 1.61, and 2.01

Author:	Driver, Cornelius
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L56D04
Link:	https://digital.library.unt.edu/ark:/67531/metadc61132/