Aerodynamic Characteristics at Mach Numbers From 2.5 to 3.5 of a Canard Bomber Configuration Designed for Supersonic Cruise Flight

Author:	Carmel, Melvin M.
Additional Authors:	Kelly, Thomas C.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L58G16
Link:	https://digital.library.unt.edu/ark:/67531/metadc64406/