Flutter investigation at low speed of a 40 degree sweptback wing with pylon-mounted stores, tested as a semispan-cantilever wing and as a full-span wing on a towed airplane model

Author:	Martina, Albert P.
Year:	1956
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L56F14A
Series:	NACA research memorandum ;
Report Number:	L56F14A
Subjects:	Charts, diagrams, etc
	Airplanes--Wings, Swept-back
	Flutter (Aerodynamics)
	Airplanes--Fuel tanks
Link:	https://hdl.handle.net/2027/mdp.39015086466045