Experimental Study of the Effects of Finite Surface Disturbances and Angle of Attack on the Laminar Boundary Layer of an NACA 64A010 Airfoil With Area Suction

Author: Schwartzberg, Milton A.
Year: 1952
Document Type: N/A
Series: NACA Technical Notes
Report Number: NASA-TM-79830, NACA-TN-2796
Link: https://digital.library.unt.edu/ark:/67531/metadc53335/

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