Investigation of the aerodynamic characteristics of the NACA RM-10 missile (with fins) at a Mach number of 1.62 in the Langley 9-inch supersonic tunnel

Author:	Coletti, Donald E.
Year:	1952
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L52J23a
Series:	National Advisory Committee for Aeronautics research memorandum ;
Report Number:	L52J23a
Subjects:	Aerodynamics, Supersonic
	Guided missiles--Aerodynamics
Link:	https://hdl.handle.net/2027/mdp.39015086465138