Longitudinal-control effectiveness and downwash characteristics at a Mach number of 1.24 of a 1/30-scale semispan model of the Bell X-5 airplane as determined by the NACA wing-flow method

Author:	Sawyer, Richard H.
Additional Authors:	Kennedy, Robert M.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L50K15
Link:	https://digital.library.unt.edu/ark:/67531/metadc58759/