Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds

Author:	Guy, Lawrence D.
Year:	1954
Document Type:	MAIN
SUDOC:	Y 3.N 21/5:15/L54G12a
Series:	NACA research memorandum ;
Report Number:	L54G12a
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Flaps (Airplanes)
	Airplanes--Wings, Triangular
	Aerodynamics, Transonic
	Aerodynamics, Supersonic
	Trailing edges (Aerodynamics)
	Hinge moments (Aerodynamics)
	Airplanes--Control surfaces
Link:	https://hdl.handle.net/2027/mdp.39015095100817