Lift and moment characteristics at subsonic Mach numbers of four 10-percent-thick airfoil sections of varying trailing-edge thickness

Author:	Summers, James L.
Year:	1950
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A50J09
Link:	https://digital.library.unt.edu/ark:/67531/metadc58629/