Two-Dimensional Wind-Tunnel Investigation of Modified NACA 65(112)-111 Airfoil with 35-Percent-Chord Slotted Flap to Determine Optimum Flap Configuration at Reynolds Number of 2.4 Million

Author:	Racisz, Stanley F.
Year:	1947
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L7A02
Link:	https://digital.library.unt.edu/ark:/67531/metadc64449/