Theoretical investigation of longitudinal response characteristics of a swept-wing fighter airplane having a normal acceleration control system and a comparison with other types of systems

Author:	Stokes, Fred H.
Year:	1954
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3191
Link:	https://digital.library.unt.edu/ark:/67531/metadc57313/