A Wind-Tunnel Investigation of the Effects of Conical Camber for an Airplane Configuration Having a Triangular Wing of Aspect Ratio 2.2

Author:	Phelps, E. Ray
Year:	1957
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A57A10
Link:	https://digital.library.unt.edu/ark:/67531/metadc53055/