Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick tapered, unswept wing

Author:	English, Roland D.
Year:	1954
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L54F29A
Series:	NACA research memorandum ;
Report Number:	L54F29A
Subjects:	Charts, diagrams, etc
	Airplanes--Wings
	Drag (Aerodynamics)
	Rolling (Aerodynamics)
	Airplanes--Fuel tanks
	Ailerons
Link:	https://hdl.handle.net/2027/mdp.39015086465633