Additional Results in a Free-Flight Investigation of Control Effectiveness of Full-Span, 0.2-Chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Aspect Ratio, Taper, and Section Thickness Ratio

Author:	Sandahl, Carl A.
Year:	1948
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L7L01
Link:	https://digital.library.unt.edu/ark:/67531/metadc58183/