Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack

Author:	McDearmon, Russell W.
Additional Authors:	Jones, Robert A.
Year:	1956
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L56F13a
Series:	NACA research memorandum ;
Report Number:	L56F13a
Subjects:	Charts, diagrams, etc
	Wind tunnel testing
	Airplanes--Wings, Triangular
	Airplanes--Models--Testing
	Airplanes--Models--Wings
	Rolling (Aerodynamics)
	Airplanes--WIngs, Triangular
Link:	https://hdl.handle.net/2027/mdp.39015086490169