Effects of Components and Various Modifications on the Drag and the Static Stability and Control Characteristics of a 42 Deg Swept-Wing Fighter-Airplane Model at Mach Numbers of 1.60 to 2.50

Author:	Church, James D.
Year:	1959
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L57K01
Link:	https://digital.library.unt.edu/ark:/67531/metadc53080/