Investigation at a Mach Number of 1.93 to Determine Lift, Drag, Pitching-Moment, and Average Downwash Characteristics for Several Missile Configurations Having Rectangular Wings and Tails of Various Spans

Author:	Grigsby, Carl E.
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50I08
Link:	https://digital.library.unt.edu/ark:/67531/metadc58611/