An Investigation at Transonic Speeds of the Effects of Control Chord and Span on the Control Characteristics of a Tapered Wedge-Type Wing of Aspect Ratio 2.5: Transonic-Bump Method

Author:	Vogler, Raymond D.
Additional Authors:	Lockwood, Vernard E.
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51G03
Link:	https://digital.library.unt.edu/ark:/67531/metadc58943/