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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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