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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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