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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