Aerodynamic characteristics of a spoiler-slot-deflector control on a 45©� sweptback wing at Mach numbers of 1.61 and 2.01

Author:	Lord, Douglas R.
Additional Authors:	Moring, Robert.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L57E16A
Series:	NACA research memorandum ;
Report Number:	L57E16A
Subjects:	Charts, diagrams, etc
	Aerodynamics
	Wind tunnel testing
	Airplanes--Models--Testing
	Airplanes--Control surfaces
	Spoilers (Airplanes)
	Airplanes--Wngs, Swept-back
Link:	https://hdl.handle.net/2027/mdp.39015086466151