Effects of a Detached Tab on the Hinge-Moment and Effectiveness Characteristics of an Unswept Trailing-Edge Control on a 60 Degree Delta Wing at Mach Numbers From 0.75 to 1.96

Author:	Morris, Odell A.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55B15
Link:	https://digital.library.unt.edu/ark:/67531/metadc61254/