Flight Investigation at Low Angles of Attack to Determine the Longitudinal Stability and Control Characteristics of a Cruciform Canard Missile Configuration With a Low-Aspect-Ratio Wing and Blunt Nose at Mach Numbers From 1.2 to 2.1

Author:	Brown, Clarence A., Jr.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55K16
Link:	https://digital.library.unt.edu/ark:/67531/metadc62339/