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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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