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The effect of Reynolds number on the stalling characteristics and pressure distributions of four moderately thin airfoil sections
Author:
McCullough, George B.
Year:
1955
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-3524
Link:
https://digital.library.unt.edu/ark:/67531/metadc57640/
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