Effects of compressibility on lift and load characteristics of a tapered wing of NACA 64-210 airfoil sections up to a Mach number of 0.60

Author:	West, F. E.
Additional Authors:	Himka, T.
Year:	1949
Document Type:	TNNA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:6/1877
Series:	National Advisory Committee for Aeronautics ;
Report Number:	no. 1877
Subjects:	Lift (Aerodynamics)
	Wind tunnel testing
	Pitching (Aerodynamics)
	Aerofoils
Link:	https://hdl.handle.net/2027/mdp.39015086493858