Test of NACA 66,2-116, a =0.6 airfoil section fitted with pressure balanced and slotted flaps for the wing of the XP-63 airplane

Author:	Underwood, William J.
Additional Authors:	Abbott, Frank T.
Year:	1942
Document Type:	MAIN
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:11/L701
Series:	Wartime Report / National Advisory Committee for Aeronautics ;
Report Number:	no. L701
Subjects:	Charts, diagrams, etc
	Lift (Aerodynamics)
	Aerodynamic load
	Wind tunnel testing
	Drag (Aerodynamics)
	Hinge moments (Aerodynamics)
	Aerofoils--Testing
	Flaps (Aerodynamics)
Link:	https://hdl.handle.net/2027/mdp.39015095014844