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Pressure-Distribution Investigation of an N.A.C.A. 0009 Airfoil With a 50-Percent-Chord Plain Flap and Three Tabs
Author:
Street, William G.
Year:
1939
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-734
Link:
https://digital.library.unt.edu/ark:/67531/metadc54501/
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