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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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