Free-flight measurements of the rolling effectiveness and drag of trailing-edge spoilers on a tapered sweptback wing at Mach numbers between 0.6 and 1.4

Author:	Schult, Eugene D.
Additional Authors:	Fields, E. M.
Year:	1954
Document Type:	MAIN
SUDOC:	Y 3.N21/5:15/L53L14a
Series:	NACA research memorandum ;
Report Number:	L53L14a
Subjects:	Mach number
	Spoilers (Airplanes)--Performance
	Airplanes--Wings, Swept-back--Handling characteristics
Link:	https://hdl.handle.net/2027/mdp.39015095100775