Effects of subsonic Mach number on the forces and pressure distributions on four NACA 64A-series airfoil sections at angles of attack as high as 28 degrees

Author: Stivers, Louis S , Jr
Year: 1954
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-3162
Link: https://digital.library.unt.edu/ark:/67531/metadc57054/

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