Investigation of transonic flutter characteristics of a thin 10 degree sweptback wing having an aspect ratio of 4 and a taper ratio of 0.6

Author:	Jones, George W.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L56L14A
Series:	NACA research memorandum ;
Report Number:	L56L14A
Subjects:	Charts, diagrams, etc
	Airplanes--Wings, Swept-back
	Aerodynamics, Transonic
	Aerofoils--Testing
	Flutter (Aerodynamics)
Link:	https://hdl.handle.net/2027/mdp.39015086466078