Collection and summary of flap-type-aileron rolling-effectiveness data at zero lift as determined by rocket-powered model tests at Mach numbers between 0.6 and 1.6

Author:	Strass, H. Kurt
Additional Authors:	Fields, E. M., Stephens, Emily W.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55F14
Link:	https://digital.library.unt.edu/ark:/67531/metadc61495/