An experimental investigation at subsonic and supersonic speeds of the torsional damping characteristics of a constant-chord control surface of an aspect ratio 2 triangular wing

Author:	Reese, David E., Jr.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A53D27
Link:	https://digital.library.unt.edu/ark:/67531/metadc59558/