Influence of fuselage and canard-type control surface on the flow field adjacent to a rearward fuselage station at a Mach number of 2.0 : data presentation

Author:	Obery, Leonard J.
Additional Authors:	Fradenburgh, Evan A.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E51K05
Link:	https://digital.library.unt.edu/ark:/67531/metadc59257/