Effects of conical camber on the lift, drag, and pitching-moment characteristics of a triangular wing of aspect ratio 3.0

Author:	Peterson, Victor L.
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A56L18
Link:	https://digital.library.unt.edu/ark:/67531/metadc63766/