Longitudinal Frequency-Response and Stability Characteristics of the Douglas D-558-II Airplane as Determined From Transient Response to a Mach Number of 0.96

Author:	Holleman, Euclid C.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L52E02
Link:	https://digital.library.unt.edu/ark:/67531/metadc59160/