Analysis of longitudinal stability and trim of the Bell X-1 airplane at a lift coefficient of 0.3 to Mach numbers near 1.05

Author:	Drake, Hubert M.
Additional Authors:	Carden, John R.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51H01
Link:	https://digital.library.unt.edu/ark:/67531/metadc58887/