An investigation of a supersonic aircraft configuration having a tapered wing with circular-arc sections and 40 degree sweepback : aerodynamic characteristics of the configuration equipped with a canard control surface at a Mach number of 1.89

Author:	Spearman, M. Leroy
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L54H19
Link:	https://digital.library.unt.edu/ark:/67531/metadc60627/