Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4

Author:	Lundstrom, Reginald R.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L57A31a
Series:	NACA research memorandum ;
Report Number:	L57A31a
Subjects:	Charts, diagrams, etc
	Aerodynamics, Supersonic
	Aspect ratio (Aerofoils)
	Rockets (Aeronautics)--Testing
	Stability of rockets
	Rockets (Aeronautics)--Models
Link:	https://hdl.handle.net/2027/mdp.39015086490490