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Investigation of NACA 65(sub 112) A111 (approx.) airfoil with 0.35-chord slotted flap at Reynolds numbers up to 25 million
Author:
Racisz, Stanley F.
Year:
1947
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1463
Link:
https://digital.library.unt.edu/ark:/67531/metadc54268/
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