Flight measurements of directional stability to a Mach number of 1.48 for an airplane tested with three different vertical tail configurations

Author:	Drake, Hubert M
Additional Authors:	Finch, Thomas W
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-H55G26
Link:	https://digital.library.unt.edu/ark:/67531/metadc61583/