Wind-tunnel investigation of the effect of clipping the tips of triangular wings of different thickness, camber, and aspect ratio - transonic bumb method

Author:	Emerson, Horace F.
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A53L03
Link:	https://digital.library.unt.edu/ark:/67531/metadc60329/