Effect on longitudinal stability and control characteristics of a Boeing B-29 airplane of variations in stick-force and control-rate characteristics obtained through use of a booster in the elevator-control system

Author:	Mathews, Charles W.
Additional Authors:	Talmage, Donald B.
Year:	1950
Document Type:	N/A
Series:	NACA Technical Reports
Report Number:	NACA-TR-1076
Link:	https://digital.library.unt.edu/ark:/67531/metadc60436/