Two-dimensional wind-tunnel investigation of a 6-percent-thick symmetrical circular-arc airfoil section with leading-edge and trailing-edge high-lift devices deflected in combination

Author:	Nuber, Robert J.
Year:	1949
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L9G20
Link:	https://digital.library.unt.edu/ark:/67531/metadc58290/