Aerodynamic characteristics of the NACA 64-010 and 0010-1.10 40/1.051 airfoil sections at Mach numbers from 0.30 to 0.85 and Reynolds numbers from 4.0 x 10(exp. 6) to 8.0 x 10(exp. 6)

Author: Loftin, Laurence K., Jr.
Year: 1954
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3244
Link: https://digital.library.unt.edu/ark:/67531/metadc57121/

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