Static and dynamic-rotary stability derivatives of an airplane model with an unswept wing and a high horizontal tail at Mach numbers of 2.5, 3.0, and 3.5

Author:	Lampkin, Bedford A.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A58F17
Link:	https://digital.library.unt.edu/ark:/67531/metadc64332/