Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35©�, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method

Author:	Thompson, Robert F.
Year:	1950
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L9L12a
Series:	NACA research memorandum ;
Report Number:	L9L12a
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Flaps (Airplanes)
	Airplanes--Wings, Swept-back
	Airplanes--Control
	Airplanes--Models--Wings
	Aerofoils--Testing
	Airplanes--Control surfaces
Link:	https://hdl.handle.net/2027/mdp.39015086490557