A theoretical investigation of the influence of auxiliary damping in pitch on the dynamic characteristics of a proportionally controlled supersonic canard missile configuration

Author:	Nelson, Walter C
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50F30
Link:	https://digital.library.unt.edu/ark:/67531/metadc58558/