Longitudinal and lateral aerodynamic characteristics at combined angles of attack and sideslip of a generalized missile model having a rectangular wing at a Mach number of 4.08

Author:	Smith, Fred M.
Additional Authors:	Ulmann, Edward F.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L58E26
Link:	https://digital.library.unt.edu/ark:/67531/metadc64289/