Experimental Static Aerodynamic Forces and Moments at Low Speed on a Missile Model During Simulated Launching From the 25-Percent-Semispan and Wing-Tip Location of a 45 Degree Sweptback Wing-Fuselage Combination

Author:	Alford, William J., Jr.
Additional Authors:	Silvers, H. Norman
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55D20
Link:	https://digital.library.unt.edu/ark:/67531/metadc61270/