Pressure Distributions and Force Tests of an NACA 65-210 Airfoil Section With a 50-Percent-Chord Flap

Author: Klein, Milton M.
Year: 1947
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-1167
Link: https://digital.library.unt.edu/ark:/67531/metadc55231/

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