Static Longitudinal and Lateral Stability and Control Characteristics of a Model of a Swept-Wing Fighter-Bomber-Type Airplane With a Top Inlet at Mach Numbers From 1.6 to 2.35

Author:	Gnos, A. Vernon
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A57K20
Link:	https://digital.library.unt.edu/ark:/67531/metadc64226/