Experimental determination of damping in pitch of swept and delta wings at supersonic Mach numbers

Author:	Moore, John A.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L57G10A
Series:	NACA research memorandum ;
Report Number:	L57G10A
Subjects:	Charts, diagrams, etc
	Pitching (Aerodynamics)
	Airplanes--Wings, Swept-back
	Airplanes--Wings, Triangular
	Aerodynamics, Supersonic
	Airplanes--Wings--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086466177