Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4

Author:	Knechtel, Earl D.
Additional Authors:	Andrea, Arvid N.
Year:	1956
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/A56H31
Series:	NACA research memorandum ;
Report Number:	A56H31
Subjects:	Rockets (Aeronautics)
	Charts, diagrams, etc
	Cylinders--Aerodynamics
	Lift (Aerodynamics)
	Pitching (Aerodynamics)
	Drag (Aerodynamics)
	Cone--Aerodynamics
Link:	https://hdl.handle.net/2027/mdp.39015086429795