Aerodynamic characteristics of a cruciform-wing missile with canard control surfaces and of some very small span wing-body missiles at a Mach number of 1.41

Author:	Spearman, M. Leroy
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L54B11
Link:	https://digital.library.unt.edu/ark:/67531/metadc60170/