Effects of modifications to a control surface on a 6-percent-thick unswept wing on the transonic control-surface flutter derivatives

Author:	Wyss, John A.
Additional Authors:	Sorenson, Robert M.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A58B04
Link:	https://digital.library.unt.edu/ark:/67531/metadc64119/