Investigation at Mach Numbers of 1.62, 1.93, and 2.41 of the Effect of Oscillation Amplitude on the Damping in Pitch of Delta-Wing-Body Combinations

Author:	Henderson, Arthur, Jr.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53H25
Link:	https://digital.library.unt.edu/ark:/67531/metadc59757/