Wing-flow tests of a triangular wing of aspect ratio two 1: effectiveness of several types of trailing-edge flaps on flat-plate models

Author:	Rathert, George A., Jr.
Year:	1947
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A7G18
Link:	https://digital.library.unt.edu/ark:/67531/metadc58153/