Lateral Stability Characteristics at Low Lift Between Mach Numbers of 0.85 and 1.15 of a Rocket-Propelled Model of a Supersonic Airplane Configuration Having a Tapered Wing With Circular-Arc Sections and 40 Degrees Sweepback

Author:	D'Aiutolo, Charles T.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55A31
Link:	https://digital.library.unt.edu/ark:/67531/metadc61131/