Pressure-distribution investigation on an NACA 0009 airfoil with a 30-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-759
Link: https://digital.library.unt.edu/ark:/67531/metadc54625/

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