Wind-tunnel tests of a blunt-nose aileron with beveled trailing edge on an NACA 66(215)-216 airfoil with several modification of aileron nose and adjacent airfoil contour

Author:	Bird, J. D.
Year:	1945
Document Type:	MAIN
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:11/L105
Series:	Wartime Report / National Advisory Committee for Aeronautics ;
Report Number:	no. L105
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Trailing edges (Aerodynamics)
	Aerofoils
	Ailerons
Link:	https://hdl.handle.net/2027/mdp.39015095014687