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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