Free-flight measurements of some effects of aileron span, chord, and deflection and of wing flexibility on the rolling effectiveness of ailerons on sweptback wings at Mach numbers between 0.8 and 1.6

Author:	Schult, Eugene D.
Additional Authors:	Strass, H. Kurt
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51K16
Link:	https://digital.library.unt.edu/ark:/67531/metadc59857/