Free-flight experience of the lateral stability characteristics at low lift of a 45 degree swept-wing rocket-propelled model equipped with a nonlinear yaw-rate damper system at Mach numbers from 0.76 to 1.73

Author:	D'Aiutolo, Charles T.
Additional Authors:	Willoughby, William W.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L56L18
Link:	https://digital.library.unt.edu/ark:/67531/metadc64183/