Component tests to determine the aerodynamic characteristics of an all-moveable 70 degree delta canard-type control in the presence of a body at a Mach number of 1.61

Author:	Spearman, M. Leroy
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53I03
Link:	https://digital.library.unt.edu/ark:/67531/metadc59873/