Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0 degrees to 20 degrees at high subsonic speeds

Author:	Daley, Bernard N.
Year:	1955
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3424
Link:	https://digital.library.unt.edu/ark:/67531/metadc57708/