Longitudinal Frequency-Response Characteristics of the Douglas D-558-I Airplane as Determined From Experimental Transient-Response Histories to Mach Number of 0.90

Author:	Angle, Ellwyn E.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51K28
Link:	https://digital.library.unt.edu/ark:/67531/metadc59925/