Aerodynamic characteristics of NACA 0012 airfoil section at angles of attack from 0 degrees to 180 degrees

Author:	Critzos, Chris C.
Additional Authors:	Heyson, Harry H.
Year:	1955
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-3361
Link:	https://digital.library.unt.edu/ark:/67531/metadc56017/