Investigation in the Langley 19-foot pressure tunnel of two wings of NACA 65-210 and 64-210 airfoil sections with various type flaps

Author:	Sivells, James C.
Additional Authors:	Spooner, Stanley H.
Year:	1948
Document Type:	TNNA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:6/1579
Series:	National Advisory Committee for Aeronautics technical note ;
Report Number:	no. 1579
Subjects:	Lift (Aerodynamics)
	Wind tunnel testing
	Flaps (Airplanes)
	Aerofoils
Link:	https://hdl.handle.net/2027/mdp.39015086493437