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Two-dimensional wind-tunnel investigation of an approximately 14-percent-thick NACA 66-series-type airfoil section with a double slotted flap
Author:
Braslow, Albert L.
Year:
1946
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1110
Link:
https://digital.library.unt.edu/ark:/67531/metadc54964/
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