Some effects of aeroelasticity and sweepback on the rolling effectiveness and drag of a 1/11-scale model of the Bell X-5 airplane wing at Mach numbers from 0.6 to 1.5

Author:	English, Roland D
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53I18b
Link:	https://digital.library.unt.edu/ark:/67531/metadc54679/