Rocket-powered-model investigation of the effects of aeroelasticity on the rolling effectiveness of an 8.06-percent-scale McDonnell F3H-1 airplane wing at Mach numbers from 0.5 to 1.4 : TED No. NACA DE 351

Author:	English, Roland D.
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-SL54D12
Link:	https://digital.library.unt.edu/ark:/67531/metadc60408/