Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60©� delta wing at Mach numbers from 0.75 to 1.96

Author:	Guy, Lawrence D.
Additional Authors:	Brown, Hoyt V.
Year:	1955
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L54K16a
Series:	NACA research memorandum ;
Report Number:	L54K16a
Subjects:	Airplanes--Wings, Triangular
	Trailing edges (Aerodynamics)
	Hinge moments (Aerodynamics)
	Trailing edge flaps
	Airplanes--Control systems--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086506998