Static lateral and directional stability and control characteristics of a 1/15-scale model of the Grumman F11F-1 airplane at Mach numbers of 1.41, 1.61, and 2.01 : TED No. NACA DE 390

Author:	Robinson, Ross B
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-SL56J10
Link:	https://digital.library.unt.edu/ark:/67531/metadc62905/