Some effects of aircraft configuration on static longitudinal and directional stability characteristics at supersonic Mach numbers below 3

Author:	Spearman, M. Leroy.
Additional Authors:	Henderson, Arthur,
Year:	1959
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L55L15a
Series:	NACA research memorandum ;
Report Number:	L55L15a
Subjects:	Stability of airplanes, Longitudinal
	Aerodynamics, Supersonic
	Stability of airplanes, Lateral
Link:	https://hdl.handle.net/2027/mdp.39015086507061