Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 to 20 degrees at high subsonic speeds

Author:	Daley, Bernard N.
Additional Authors:	Lord, Douglas R.
Year:	1949
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L9E19
Series:	NACA research memorandum ;
Report Number:	L9E19
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Angle of attack (Aerodynamics)
	Schlieren photography
	Aerofoils--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086464487