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Wind-tunnel investigation of the boundary layer on an NACA 0009 airfoil having 0.25- and 0.50- airfoil chord plain sealed flaps
Author:
Brewer, Jack D.
Year:
1948
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1574
Link:
https://digital.library.unt.edu/ark:/67531/metadc54904/
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