High-Speed Wind-Tunnel Tests of an NACA 0009-64 Airfoil Having a 33.4-Percent-Chord Flap With an Overhang 20.1 Percent of the Flap Chord

Author:	Stevenson, David B.
Year:	1947
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-1417
Link:	https://digital.library.unt.edu/ark:/67531/metadc54291/