Experimental investigation of an NACA 64A010 airfoil section with 41 suction slots on each surface for control of laminar boundary layer

Author: Burrows, Dale L
Year: 1952
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2644
Link: https://digital.library.unt.edu/ark:/67531/metadc56505/

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