Flight Determination of the Drag and Longitudinal Stability and Control Characteristics of a Rocket-Powered Model of a 60 Degrees Delta-Wing Airplane From Mach Numbers 0.75 to 1.70

Author:	Mitcham, Grady L.
Additional Authors:	Crabill, Norman L.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51I04
Link:	https://digital.library.unt.edu/ark:/67531/metadc59125/