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Aerodynamic characteristics of 15 NACA airfoil sections at seven Reynolds numbers from 0.7 x 10(exp 6) to 9.0 x 10(exp 6)
Author:
Loftin, Laurence K., Jr.
Year:
1949
Document Type:
N/A
Series:
NACA Technical Notes
Report Number:
NACA-TN-1945
Link:
https://digital.library.unt.edu/ark:/67531/metadc55250/
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