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Pressure-distribution investigation of an NACA 0009 airfoil with an 80-percent-chord plain flap and three tabs
Author:
Ames, Milton B., Jr.
Year:
1940
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-761
Link:
https://digital.library.unt.edu/ark:/67531/metadc54636/
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