Aerodynamic coefficients for an oscillating airfoil with hinged flap, with tables for a Mach number of 0.7

Author: Turner, M. J.
Year: 1950
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2213
Link: https://digital.library.unt.edu/ark:/67531/metadc55603/

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